Garmin Diamond Da40 Users Manual

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2015-01-29

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G1000

G1000 Pilot’s Guide

Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282

Integrated Flight Deck
Pilot’s Guide

Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138

Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251

www.garmin.com

Diamond
DA40/40F

Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099

190-00592-06
Revision A

System Software 0321.20 or later

Untitled-1 1

11/13/2007 9:15:37 AM

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

EIS

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

Copyright © 2006-2009 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0321.20 or later for the Diamond DA40 or DA40F. Some differences in
operation may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200
Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411
Fax: 503/364.2138
Garmin (Europe) Ltd., Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K
Tel: 44/0870.8501241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®, and SafeTaxi® are trademarks of Garmin
Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.; Becker® is a registered trademark of Becker
Flugfunkwerk GmbH; NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM Satellite Radio, Inc.; and
Stormscope® is a registered trademark of L-3 Communications.

March 2009

Printed in the U.S.A.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Limited Warranty
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made
at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty
does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED
OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR
PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole
discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit
the Garmin Website at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

Warnings, Cautions, and Notes

WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the

G1000 Pilot’s Guide documentation. Thoroughly practice basic operation prior to actual use. During flight
operations, carefully compare indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any
discrepancies before continuing navigation.
WARNING: The Garmin G1000 has a very high degree of functional integrity. However, the pilot must

recognize that providing monitoring and/or self-test capability for all conceivable system failures is not
practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication
shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING: The United States government operates the Global Positioning System and is solely responsible

for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy
and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and

could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be

relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function.

The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use
in applications requiring a certified terrain awareness system. Terrain data is obtained from third party
sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: Do not use outdated database information. Databases used in the G1000 System must be updated

regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Warnings, Cautions, and Notes

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is

intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually

acquiring traffic. The aircraft should be maneuvered based only upon ATC guidance or positive visual
acquisition of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather penetration. Weather information

provided by the GDL 69/69A is approved only for weather avoidance, not penetration.
Warning: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent

delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for
short-range weather avoidance.
WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm

penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather
avoidance, not penetration.
WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate

a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identifi ed as severe or giving
an intense radar echo.”
WARNING: Because of anomalies in the earth’s magnetic field, operating the G1000 within the following

areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south
of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An
area south of 55° South latitude between longitude 120º East and 165º East.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by

an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty
and the pilot’s authority to operate this device under FAA/FCC regulations.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very

sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

iii

Warnings, Cautions, and Notes

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms

that can cause isolated discharge points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after
the screen has been cleared.
NOTE: All visual depictions contained within this document, including screen images of the G1000 panel

and displays, are for example only, are subject to change, and may not reflect the most current G1000
System. Depictions of equipment may differ slightly from the actual equipment.
NOTE: The GDU 1040/1042/1044 PFD/MFD may require a warm-up time of up to 30 minutes when exposed

to -40˚C for an extended period. A warm-up time of up to 15 minutes may be required when exposed to
-30˚C for an extended period.
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions:

(1) this device may not cause harmful interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. For additional information, refer to the website at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 feet
away from the source of the interference should alleviate the condition.

NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Revision Information
Record of Revisions
Part Number
190-00592-00
190-00592-01
190-00592-02

Revision
A
A
A

Date
11/10/05
6/16/06
7/20/06

190-00592-03

4/20/07

190-00592-04
190-00592-05
190-00592-06

A
A
A

12/04/07
03/31/08
03/25/09

190-00592-06 Rev. A

Page Range
Description
i – I-6
Optional fuel pressure gauge information added
i – I-4
GFC 700 information added
i – I-4
TAWS information added
GDL 69A crew muting information added
i – I-6
EIS updated
Airways information added
WAAS information added
VNV information added
Charts information added
Stormscope information added
TAS600 information added
i – I-6
KAP 140 Autopilot annunciations added
i – I-6
Synthetic Vision System information added
i – I-6
Updated to GDU Software 9.14

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

Table of Contents

1.1
1.2
1.3
1.4

1.5

1.6

1.7

Section 1 System overview
Line Replaceable Units............................................ 2
Secure Digital (SD) Cards........................................ 7
System Power-up...................................................... 8
System Operation..................................................... 9
Display Operation. ........................................................ 9
G1000 System Annunciations....................................... 10
System Status............................................................. 11
AHRS Operation.......................................................... 13
GPS Receiver Operation............................................... 14
G1000 Controls....................................................... 18
PFD/MFD Controls....................................................... 18
Softkey Function. ........................................................ 20
Accessing G1000 Functionality............................ 27
Menus. ...................................................................... 27
Data Entry.................................................................. 27
Page Groups............................................................... 29
System Settings. ......................................................... 33
Timers........................................................................ 38
Display Backlighting.............................................. 41

Section 2 Flight Instruments
2.1 Flight Instruments.................................................. 46
Airspeed Indicator....................................................... 46
Attitude Indicator........................................................ 48
Altimeter.................................................................... 49
Vertical Speed Indicator (VSI). ...................................... 51
Vertical Deviation........................................................ 52
Horizontal Situation Indicator (HSI)............................... 53
Course Deviation Indicator (CDI)................................... 58
2.2 Supplemental Flight Data..................................... 65
Outside Air Temperature. ............................................. 65
Wind Data.................................................................. 67
Vertical Navigation (VNV) Indications. .......................... 68
2.3 PFD Annunciations and Alerting Functions......... 69
System Alerting........................................................... 69
Marker Beacon Annunciations...................................... 70
Traffic Annunciation. ................................................... 70
TAWS Annunciations. .................................................. 71
Altitude Alerting. ........................................................ 72
Low Altitude Annunciation........................................... 72
Minimum Descent Altitude/Decision Height Alerting....... 73

2.4 Abnormal Operations............................................ 74
Abnormal GPS Conditions............................................ 74
Unusual Attitudes. ...................................................... 75
3.1
3.2
3.3
3.4

Section 3 Engine Indication System
EIS Display............................................................... 78
Engine Page............................................................ 80
Fuel Calculations......................................................... 82
Leaning Assist Mode.............................................. 83
EIS Display in Reversionary Mode........................ 84
Lean Display............................................................... 86
System Display............................................................ 88
Section 4 audio panel and CNS

4.1 Overview................................................................. 91
MFD/PFD Controls and Frequency Display...................... 92
Audio Panel Controls................................................... 94
4.2 COM Operation....................................................... 96
COM Transceiver Selection and Activation. .................... 96
COM Transceiver Manual Tuning................................... 97
Quick-Tuning and Activating 121.500 MHz.................... 98
Auto-Tuning the COM Frequency.................................. 99
Frequency Spacing. ................................................... 103
Automatic Squelch.................................................... 104
Volume. ................................................................... 104
4.3 NAV Operation...................................................... 105
NAV Radio Selection and Activation............................ 105
NAV Receiver Manual Tuning. .................................... 106
Auto-Tuning a NAV Frequency from the MFD............... 108
Marker Beacon Receiver. ........................................... 113
ADF/DME Tuning....................................................... 114
4.4 GTX 33 Mode S Transponder............................... 118
Transponder Controls. ............................................... 118
Transponder Mode Selection. ..................................... 119
Entering a Transponder Code...................................... 122
IDENT Function......................................................... 123
4.5 Additional Audio Panel Functions...................... 124
Power-Up. ................................................................ 124
Mono/Stereo Headsets. ............................................. 124
Speaker.................................................................... 124
Intercom. ................................................................. 125
Passenger Address (PA) System. ................................. 127
Clearance Recorder and Player................................... 127

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Table of Contents
Entertainment Inputs................................................. 128

4.6 Audio Panel Preflight Procedure........................ 129
4.7 Abnormal Operation............................................ 130
Stuck Microphone..................................................... 130
COM Tuning Failure................................................... 130
Audio Panel Fail-Safe Operation. ................................ 130
Reversionary Mode. .................................................. 130
5.1
5.2

5.3

5.4
5.5
5.6

Section 5 Flight Management
Introduction.......................................................... 131
Navigation Status Box............................................... 133
Using Map Displays.............................................. 134
Map Orientation. ...................................................... 134
Map Range............................................................... 136
Map Panning............................................................ 138
Measuring Bearing and Distance. ............................... 143
Topography. ............................................................. 144
Map Symbols............................................................ 147
Airways.................................................................... 153
Track Vector.............................................................. 155
Wind Vector.............................................................. 156
Nav Range Ring........................................................ 157
Fuel Range Ring........................................................ 158
Field of View (SVS). ................................................... 159
Waypoints.............................................................. 160
Airports.................................................................... 161
Intersections............................................................. 167
NDBs. ...................................................................... 169
VORs........................................................................ 171
User Waypoints......................................................... 173
Airspaces............................................................... 179
Direct-to-Navigation . ......................................... 183
Flight Planning...................................................... 189
Flight Plan Creation................................................... 190
Adding Waypoints to an Existing Flight Plan................ 195
Adding Airways to a Flight Plan.................................. 197
Adding Procedures to a Stored Flight Plan................... 200
Flight Plan Storage.................................................... 207
Flight Plan Editing..................................................... 209
Along Track Offsets. .................................................. 212
Parallel Track. ........................................................... 214
Activating a Flight Plan Leg........................................ 217
Inverting a Flight Plan. .............................................. 218

190-00592-06 Rev. A

Flight Plan Views....................................................... 219
Closest Point of FPL................................................... 221

5.7 Vertical Navigation.............................................. 222
Altitude Constraints. ................................................. 224
5.8 Procedures............................................................ 228
Departures. .............................................................. 228
Arrivals . .................................................................. 231
Approaches . ............................................................ 233
5.9 Trip Planning......................................................... 239
Trip Planning. ........................................................... 239
5.10 RAIM Prediction................................................... 243
5.11 Navigating a Flight Plan...................................... 247
5.12 Abnormal Operation............................................ 275
6.1

6.2

6.3

6.4

6.5

6.6

6.7

Section 6 Hazard Avoidance
XM Satellite Weather........................................... 277
Activating Services.................................................... 278
Using XM Satellite Weather Products.......................... 279
WX-500 Stormscope............................................ 306
Setting Up Stormscope on the Navigation Map............ 306
Selecting the Stormscope Page................................... 310
Terrain Proximity.................................................. 311
Displaying Terrain Proximity Data. .............................. 311
Terrain Proximity Page............................................... 314
Terrain-SVS............................................................ 316
TERRAIN-SVS Page.................................................... 320
TERRAIN-SVS Alerts................................................... 322
System Status........................................................... 325
Terrain Awareness & Warning System (TAWS).. 326
Displaying TAWS Data. .............................................. 327
TAWS-B Page............................................................ 329
TAWS Alerts.............................................................. 331
System Status........................................................... 337
Traffic Information Service (TIS)......................... 339
Displaying TRAFFIC Data............................................ 340
Traffic Map Page....................................................... 342
TIS Alerts.................................................................. 343
System Status........................................................... 345
Traffic Advisory System....................................... 348
TAS Symbology......................................................... 348
Displaying Traffic Data............................................... 349
Traffic Map Page Display Range.................................. 351
TAS Alerts................................................................. 353

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

vii

Table of Contents
TAS Voice Alerts. ....................................................... 353
System Status........................................................... 354

Section 7 Automatic Flight Control System
7.1 AFCS Controls....................................................... 358
7.2 Flight Director Operation.................................... 360
Activating the Flight Director...................................... 360
AFCS Status Box. ...................................................... 361
Command Bars......................................................... 362
Flight Director Modes................................................ 362
7.3 Vertical Modes...................................................... 363
Pitch Hold Mode (PIT)................................................ 364
Selected Altitude Capture Mode (ALTS). ...................... 365
Altitude Hold Mode (ALT)........................................... 366
Vertical Speed Mode (VS)........................................... 367
Flight Level Change Mode (FLC). ................................ 368
Vertical Navigation Modes (VPTH, ALTV). .................... 370
Glidepath Mode (GP) (WAAS only). ............................ 375
Glideslope Mode (GS)................................................ 377
Go Around Mode (GA)............................................... 378
7.4 Lateral Modes....................................................... 379
Roll Hold Mode (ROL)................................................ 380
Heading Select Mode (HDG)....................................... 381
Navigation Modes (GPS, VOR, LOC, BC)....................... 382
Approach Modes (GPS, VAPP, LOC).............................. 384
7.5 Autopilot Operation............................................. 386
Engaging the Autopilot.............................................. 386
Control Wheel Steering.............................................. 387
Disengaging the Autopilot. ........................................ 387
7.6 Example Flight Plan............................................. 388
Departure................................................................. 389
Intercepting a VOR Radial.......................................... 391
Flying a Flight Plan/GPS Course.................................. 392
Descent.................................................................... 393
Approach. ................................................................ 397
Go Around/Missed Approach...................................... 399
7.7 AFCS Annunciations and Alerts.......................... 401
AFCS Status Alerts..................................................... 401
Overspeed Protection. ............................................... 402
Annunciations for KAP 140 Autopilot System............... 402

8.1

8.2
8.3

8.4

8.5

8.6
8.7
8.8
8.9

Section 8 Additional Features
Synthetic Vision System (SVS) (Optional).......... 404
SVS Operation. ......................................................... 405
SVS Features............................................................. 407
Field of View............................................................. 415
SafeTaxi................................................................. 417
SafeTaxi Cycle Number and Revision........................... 420
ChartView.............................................................. 423
ChartView Softkeys. .................................................. 423
Terminal Procedures Charts........................................ 424
Chart Options........................................................... 432
Day/Night View......................................................... 438
ChartView Cycle Number and Expiration Date. ............ 440
FliteCharts............................................................. 444
FliteCharts Softkeys................................................... 444
Terminal Procedures Charts........................................ 445
Chart Options........................................................... 452
Day/Night View......................................................... 456
FliteCharts Cycle Number and Expiration Date............. 458
XM Radio Entertainment (Optional).................. 462
Activating XM Satellite Radio Services. ....................... 462
Using XM Radio........................................................ 464
Scheduler............................................................... 467
Electronic Checklists............................................ 469
Flight Data Logging............................................. 472
Abnormal Operation............................................ 474
SVS Troubleshooting.................................................. 474
Reversionary Mode. .................................................. 474
Unusual Attitudes. .................................................... 475

Appendices
Annunciations and Alerts.............................................. 479
SVS Terrain Alerts...................................................... 496
SVS Terrain Status Annunciations................................ 496
SD Card Use and Databases.......................................... 499
Glossary........................................................................... 503
Frequently Asked Questions......................................... 509
General TIS Information................................................ 513
Map Symbols.................................................................. 515
Index
Index . ...............................................................................I-1

viii

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

Section 1 System overview

FLIGHT
INSTRUMENTS

NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the GFC 700 AFCS.

The G1000 Integrated Flight Deck System presents flight instrumentation, position, navigation, communication,
and identification information using flat-panel color displays. The system is distributed across the following Line
Replaceable Units (LRUs):
• GDU 1040/1042/1044 Multi Function Display
(MFD)

• GRS 77 Attitude and Heading Reference System
(AHRS)

• GMA 1347 Audio Panel with Integrated Marker
Beacon Receiver

• GMU 44 Magnetometer
• GDL 69/69A Data Link Receiver

• GIA 63/63W Integrated Avionics Units (IAU)

• GSA 81 AFCS Servos

• GDC 74A Air Data Computer (ADC)

• GSM 85 Servo Mounts

AUDIO PANEL
& CNS

• GTX 33 Mode S Transponder
EIS

• GDU 1040 Primary Flight Display (PFD)

FLIGHT
MANAGEMENT

• GEA 71 Engine/Airframe Unit
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.
The Diamond DA40/40F may be optionally equipped with a GFC 700 Automated Flight Control System (AFCS),
providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

1.1 Line Replaceable Units

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

• GDU 1040/1042/1044 (2) – A GDU 1040 is configured as the Primary Flight Display (PFD) and a GDU 1040,
1042 or 1044 (1042/1044 for airframes equipped with the GFC 700) as a Multi Function Display (MFD). Both
displays feature 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with each other
through a High-speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet
connection to an IAU. The three GDU models are distinguished by three individual configurations of bezel
controls and are made available to accommodate a variety optional system installations.

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

• GMA 1347 – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom,
and marker beacon controls, and is installed between the displays. This unit also provides manual control of
display Reversionary Mode (red DISPLAY BACKUP button; see Section 1.4, System Operation) and communicates
with both IAUs using an RS-232 digital interface.

INDEX

APPENDICES

ADDITIONAL
FEATURES

• GIA 63/63W (2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking
all LRUs with the PFD. Each IAU contains a GPS receiver, a very high frequency (VHF) communication/
navigation/glideslope (COM/NAV/GS) receiver, and system integration microprocessors, and is paired with
the on-side display via an HSDB connection. The GIA 63W contains a GPS WAAS receiver. The IAUs are not
paired together and do not communicate with each other directly.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

GDC 74A – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature
(OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the
G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital
interface.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

• GEA 71 – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This
unit communicates with both IAUs using an RS-485 digital interface.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

• GTX 33 – The solid-state Transponder provides Modes A, C, and S capability and communicates with both IAUs
through an RS-232 digital interface.

AFCS
ADDITIONAL
FEATURES

• GRS 77 (2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors
(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field
information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation
is discussed in Section 1.4, System Operation.

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

FLIGHT
INSTRUMENTS

• GMU 44 – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to
determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with
it via an RS-485 digital interface.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

• GDL 69/69A – The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps
and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment. The
Data Link Receiver communicates with the MFD via an HSDB connection. A subscription to XM Satellite Radio
Service is required to enable Data Link Receiver capability.

• GSA 81 and GSM 85 – The GSA 81 servos are used for automatic control of pitch, pitch trim, and roll. These
units interface with each IAU.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

The GSM 85 servo mounts are responsible for transferring the output torque of the servo actuators to the
mechanical flight-control surface linkages.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

High-Speed Data Bus (Ethernet)

GMA 1347
Audio Panel

GDU 1040 (PFD)

GDU 1040/1042/1044 (MFD)

FLIGHT
INSTRUMENTS

Reversionary
Control

EIS

GDC 74A
Air Data
Computer
No. 2 GIA 63/63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope

GRS 77
AHRS
Attitude
Rate of Turn
Slip/Skid

FLIGHT
MANAGEMENT

System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
Flight Director (with GFC 700 option)
GPS Output

AUDIO PANEL
& CNS

OAT
Airspeed
Altitude
Vertical Speed

No. 1 GIA 63/63W
Integrated Avionics Unit

GPS Output

GMU 44
Magnetometer

HAZARD
AVOIDANCE

Heading

GTX 33
Transponder

Autopilot Calculations
(optional)

GSA 81
Roll Servo

Autopilot Calculations
(optional)

ADDITIONAL
FEATURES

GSA 81
Pitch Servo

AFCS

GEA 71
Engine/Airframe
Unit

GSA 81
Pitch Trim Servo

Autopilot Calculations
(optional)

APPENDICES

Figure 1-1 G1000 System Block Diagram

NOTE: The GDU 1042 and GDU 1044 are equipped with additional bezel controls and are available for use

in systems equipped with the Garmin GFC 700 Automatic Flight Control System.
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

High-Speed Data Bus (Ethernet)

No. 2 GIA 63/63W
Integrated Avionics Unit

FLIGHT
MANAGEMENT

System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope

HAZARD
AVOIDANCE

Becker
RA 3502-(1)
ADF Receiver
(optional)

Honeywell
KN 63
DME
(optional)

Avidyne
TAS600-series
Traffic Information
(optional)

GDL 69/69A

Data Link Receiver
Real-time Weather and
Digital Audio Entertainment
(subscription-based service)

L3
Stormscope

Lightning Strike and
Thunderstorm Detection
(optional)

Honeywell
KAP 140
Autopilot
(optional)

AFCS

Figure 1-2 G1000 With Optional/Additional Interfaces

NOTE: The GDU 1040 is available in systems using the Honeywell KAP 140 Autopilot.

ADDITIONAL
FEATURES

NOTE: For information on additional equipment shown in Figure 1-2, consult the applicable optional interface

INDEX

APPENDICES

user’s guide. This document assumes that the reader is already familiar with the operation of this additional
equipment.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

1.2 Secure Digital (SD) Cards

FLIGHT
INSTRUMENTS

NOTE: Ensure the G1000 System is powered off before inserting an SD card.
NOTE: Refer to Appendix B for instructions on updating databases.

EIS

The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the
display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database
and system software updates as well as terrain database storage.
Installing an SD card:

AUDIO PANEL
& CNS

1) Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card
should remain flush with the face of the display bezel.
2) To eject the card, gently press on the SD card to release the spring latch.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

SD Card Slots

AFCS
ADDITIONAL
FEATURES

Figure 1-3 Display Bezel SD Card Slots

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

1.3 System Power-up

FLIGHT
INSTRUMENTS

NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application

and emergency power supply operation.
NOTE: Refer to Appendix A for system-specific annunciations and alerts.

EIS

The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical
busses. The PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features
that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation.

AUDIO PANEL
& CNS

During system initialization, test annunciations are displayed, as shown in Figure 1-4. All system annunciations
should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also
become momentarily illuminated on the Audio Panel and the display bezels.

FLIGHT
MANAGEMENT

On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should
display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself
both while taxiing and during level flight.

HAZARD
AVOIDANCE

When the MFD powers up, the splash screen (Figure 1-5) displays the following information:
• System version

• Obstacle database name and version

• Copyright

• Terrain database name and version

• Land database name and version

• Aviation database name, version, and effective dates

Current database information includes valid operating dates, cycle number, and database type. When this
information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to
continue.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Navigation Map Page is
displayed upon pressing the key a second time. When the system has acquired a sufficient number of satellites to
determine a position, the aircraft’s current position is shown on the Navigation Map Page.

Figure 1-4 PFD Initialization

Figure 1-5 Example (DA40) MFD Power-up Splash Screen

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

1.4 System Operation

FLIGHT
INSTRUMENTS

NOTE: Refer to Appendix A for detailed descriptions of all alerts and annunciations. Refer to the Aircraft

Flight Manual (AFM) for additional information regarding pilot responses to these annunciations.
The displays are connected together via a single Ethernet bus for high-speed communication. As shown in
Figure 1-1, each IAU is connected to the on-side display. This allows the units to share information, enabling true
system integration

EIS

Display Operation
NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In Reversionary Mode, it

AUDIO PANEL
& CNS

can be adjusted from the remaining display.

FLIGHT
MANAGEMENT

In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed,
altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section
for more information). The MFD normally displays a full-color moving map with navigation information (see
the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System
(EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection.

HAZARD
AVOIDANCE
AFCS

Figure 1-6 G1000 Normal Operation
ADDITIONAL
FEATURES
APPENDICES

In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In
Reversionary Mode, all important flight information from the PFD is presented on the remaining display in the
same format as in normal operating mode, with the addition of the EIS. EIS operation while in Reversionary
Mode is discussed in the EIS Section. As when the PFD is operating normally, windows for flight planning,
nearest airports, and procedures are available. The Inset Map is moved to the right side of the display.

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

If a display fails, the appropriate IAU-display Ethernet interface is cut off. Thus, the IAU can no longer
communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to
the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup
paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is
completely automated for all LRUs and no pilot action is required.

SYSTEM
OVERVIEW

System Overview
If the system fails to detect a display problem, Reversionary Mode may be manually activated by pressing the
Audio Panel’s red DISPLAY BACKUP Button. Pressing this button again deactivates Reversionary Mode.

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

NAV1 and COM1 (provided by the
failed PFD) Flagged Invalid

DISPLAY BACKUP Button Manually Activates/
Deactivates Reversionary Mode on Both Displays

FLIGHT
MANAGEMENT

Figure 1-7 G1000 Reversionary Mode (Failed PFD)

G1000 System Annunciations

HAZARD
AVOIDANCE

When an LRU or an LRU function fails, a large red ‘X’ is typically displayed over the instrument experiencing
failed data (Figure 1-8 displays all possible flags and responsible LRUs). The G1000 System alerts the pilot
when backup paths are utilized by the LRUs. Upon G1000 power-up, certain instruments remain invalid as
equipment begins to initialize. All instruments should be operational within one minute of power-up. If any
instrument remains flagged, the G1000 should be serviced by a Garmin-authorized repair facility.

AFCS

GIA 63/63W Integrated Avionics Units

ADDITIONAL
FEATURES

GDC 74A
Air Data
Computer
Database
Mismatch in the
PFD and MFD

APPENDICES

GEA 71
Engine
Airframe Unit
OR
GIA 63/63W
Integrated
Avionics Unit

GRS 77 AHRS
OR GMU 44
Magnetometer
GIA 63/63W
Integrated
Avionics Units

INDEX

GDC 74A
Air Data
Computer
GTX 33 Transponder OR GIA 63/63W
Integrated Avionics Units
Figure 1-8 G1000 System Failure Annunciations

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

System Status

FLIGHT
INSTRUMENTS

The System Status Page displays the statuses, serial numbers, and software version numbers for all detected
system LRUs. Active LRUs are indicated by green check marks; failed, by red ‘X’s. Failed LRUs should be noted
and a service center or Garmin-authorized dealer informed.
Viewing LRU information:
1) Use the FMS Knob to select the AUX - System Status Page.
2) To place the cursor in the ‘LRU Info’ Box,

EIS

a) Press the LRU Softkey.
Or:
a) Press the MENU Key.

AUDIO PANEL
& CNS

b) With ‘Select LRU Window’ highlighted, press the ENT Key.
3) Use the FMS Knob to scroll through the box to view LRU status information.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 1-9 Example System Status Page

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
Pertinent information on all system databases is also displayed on this page. Refer to the Appendices and
Additional Features sections for more information about databases.

FLIGHT
INSTRUMENTS

Viewing database information:
1) Use the FMS Knob to select the AUX - System Status Page.
2) To place the cursor in the ‘Database’ Box,
a) Press the DBASE Softkey.
Or:
EIS

a) Press the MENU Key.
b) Highlight ‘Select Dbase Window’ and press the ENT Key.

AUDIO PANEL
& CNS

3) Use the FMS Knob to scroll through the box to view database status information.

The G1000 uses aural tones to convey the priority of airframe-specific alerts. The alerting system’s annunciation
tone may be tested from the System Status Page. Refer to the Appendices for airframe-specific alerts.
Testing the system annunciation tone:

FLIGHT
MANAGEMENT

1) Use the FMS Knob to select the AUX - System Status Page.
2) Press the ANN TEST Softkey.

Or:

HAZARD
AVOIDANCE

a) Press the MENU Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

AHRS Operation
NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy.

FLIGHT
INSTRUMENTS

The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration
calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information
from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives
appropriate combinations of information from the external sensor inputs.

unavailable

available

unavailable

FLIGHT
MANAGEMENT

le
ab

AHRS
no-GPS
Mode

ail
av

AHRS no- AHRS no-Mag/
Mag Mode
no-Air Mode
Heading Invalid

Air Data
un

available

unavailable

available

unavailable

available

Air Data

AHRS Normal
Operation

Magnetometer Data

AUDIO PANEL
& CNS

Magnetometer Data

EIS

GPS Data

Attitude/Heading Invalid

HAZARD
AVOIDANCE

Figure 1-10 AHRS Operation
AFCS
ADDITIONAL
FEATURES

Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts (refer
to Appendix A for specific AHRS alert information). Any failure of the internal AHRS inertial sensors results in
loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments).

APPENDICES

Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses
the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS
can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed
data are available and valid.
If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the
heading output on the PFD is flagged as invalid with a red ‘X’.

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Failure of the air data input has no effect on the AHRS output while AHRS is receiving valid GPS information.
Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading
information.

SYSTEM
OVERVIEW

System Overview

GPS Receiver Operation

FLIGHT
INSTRUMENTS

Each Integrated Avionics Unit (IAU) contains a GPS receiver. Internal system checking is performed to
ensure both GPS receivers are providing accurate data to the PFD. When both GPS receivers are providing
accurate data, the GPS receiver producing the better solution is used by the system. Information collected by
the specified receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX - GPS Status
Page.
Viewing GPS receiver status information:

EIS

1) Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.6 for information on
navigating MFD page groups).
2) Use the small FMS Knob to select GPS Status Page (third page in the AUX Page Group).

AUDIO PANEL
& CNS

Press the desired GPS Softkey.

FLIGHT
MANAGEMENT

3) To change the selected GPS receiver:

b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key.

Or:
a) Press the MENU Key.
Satellite Signal
Information

GPS Receiver
Status

HAZARD
AVOIDANCE

Satellite Constellation
Diagram

ADDITIONAL
FEATURES

AFCS

RAIM
Availability
Prediction

INDEX

APPENDICES

Satellite
Signal
Strength
Bars

Figure 1-11 GPS Status Page

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

For WAAS-enabled systems, GPS sensor annunciations are most often seen after system power-up when one
GPS receiver has acquired satellites before the other or one of the GPS receivers has not yet acquired a WAAS
signal. While the aircraft is on the ground, the WAAS signal may be blocked by obstructions causing one GPS
receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of
the GPS receivers temporarily losing the WAAS signal. If no failure message exists, check the GPS Status Page
and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem.

GPS receiver status

EIS

The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active
GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is
in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data
(collected continuously from the satellites) and last known position to determine the satellites that should be
in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired
for computing a solution.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

When the receiver is in the process of acquiring a 3D navigational GPS solution, 3D NAV is indicated as the
solution until the 3D differential fix has finished acquisition. Satellite-Based Augmentation System (SBAS)
status should be indicated as INACTIVE at this point. When acquisition is complete, the solution status
changes to 3D DIFF NAV and SBAS becomes active.
In certain situations, such as when the aircraft is outside or on the fringe of the WAAS or MSAS (used only
in Japan) coverage area, it may be desirable to disable WAAS or MSAS (although it is not recommended).
When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a small delay for
the GPS Status box to be updated upon WAAS and MSAS enabling/disabling.

HAZARD
AVOIDANCE

Disabling WAAS or MSAS
1) Select the GPS Status Page.
2) If necessary, press the SBAS Softkey.
3) Press the FMS Knob, and turn the large FMS Knob to hightlight ‘MSAS’ or ‘WAAS’.

AFCS

4) Press the ENT Key to uncheck the box.
5) Press the FMS Knob to remove the cursor.

ADDITIONAL
FEATURES
APPENDICES

Figure 1-12 Enable/Disable WAAS

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
RAIM Prediction

FLIGHT
INSTRUMENTS

Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency
check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to
calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0
nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of
flight, RAIM is available nearly 100% of the time.

EIS

The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM
computations predict satellite coverage within ±15 min of the specified arrival date and time. In G1000
systems with WAAS enabled, performing RAIM prediction is not necessary in most cases. However, if the
selected approach is outside the WAAS coverage area, it may be necessary to perform a RAIM prediction for
the intended approach.

AUDIO PANEL
& CNS

Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The
G1000 automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not
predicted to be available for the final approach course, the approach does not become active, as indicated by
the messages “Approach is not active”. If RAIM is not available when crossing the FAF, the missed approach
procedure must be flown.

FLIGHT
MANAGEMENT

Predicting RAIM availability:
1) Select the GPS Status Page.
2) Press the RAIM Softkey.

HAZARD
AVOIDANCE

2) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted.
3) Turn the small FMS Knob to display the Waypoint Information Window.
4) Enter the desired waypoint and press the ENT Key (refer to Section 1.6 for instructions on data entry).
Or:

AFCS

a) To use the present position, press the MENU Key.
b) With ‘Set WPT to Present Position’ highlighted, press the ENT Key.
c) Press the ENT Key to accept the waypoint entry.
ADDITIONAL
FEATURES

5) Enter an arrival time and press the ENT Key.
6) Enter an arrival date and press the ENT Key.

• ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination

• ‘COMPUTING AVAILABILITY’—RAIM calculation in progress

• ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date

• ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date

INDEX

APPENDICES

7) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one
of the following is displayed:

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

Satellite Information

FLIGHT
INSTRUMENTS

Satellites currently in view are shown at their respective positions on a satellite constellation diagram.
This sky view is always oriented north-up, with the outer circle representing the horizon, the inner circle
representing 45° above the horizon, and the center point showing the position directly overhead. Each satellite
is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification
number). Satellites whose signals are currently being used are represented by solid ovals.

EIS

The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite
coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed
for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for WAAS) below each
bar. The progress of satellite acquisition is indicated by signal bar appearance:
• No signal strength bar—Receiver is looking for the indicated satellite.

AUDIO PANEL
& CNS

• Hollow signal strength bar—Receiver has found the satellite and is collecting data. Each satellite has a 30second data transmission that must be collected (signal strength bar is hollow) before the satellite may be
used for navigation (signal strength bar becomes solid).
• Solid signal strength bar—Receiver has collected the necessary data and the satellite signal can be used.

FLIGHT
MANAGEMENT

• Checkered signal strength bar—Receiver has excluded the satellite (Fault Detection and Exclusion; FDE).
• “D” indication on signal strength bar—Satellite is being used for differential computations.
• Green signal strength bar—Satellites that are actually being used in the position calculation.
• Blue signal strength bar—Satellite is locked on but not yet being used in the position calculation.

HAZARD
AVOIDANCE

Using the current satellite signal information, they system calculates the aircraft’s GPS position, time,
altitude, ground speed, and track for the aircraft (displayed below the satellite signal accuracy measurements
for reference). The following quantities denote the accuracy of the aircraft’s GPS fix:
• Estimated Position Uncertainty (EPU)—A statistical error indication; the radius of a circle centered on an
estimated horizontal position in which actual position has 95% probability of lying

AFCS

• Horizontal Dilution of Precision (HDOP)—Measures satellite geometry quality (i.e., number of satellites
received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting
better accuracy

ADDITIONAL
FEATURES

• Horizontal and Vertical Figures of Merit (HFOM and VFOM)—Measures of horizontal and vertical position
uncertainty; the current 95% confidence horizontal and vertical accuracy values reported by the GPS
receiver

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

1.5 G1000 Controls

FLIGHT
INSTRUMENTS

The G1000 controls have been designed to simplify operation of the system and minimize workload and the
time required to access sophisticated functionality. Controls are located on the PFD and MFD bezels and Audio
Panel. PFD and MFD controls and softkeys are discussed in this section. See the Audio Panel and CNS Section
for more information about Audio Panel and NAV/COM controls. AFCS controls (on the bezel of the MFD) are
described in the AFCS section.

EIS

PFD/MFD Controls
2

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

AFCS

ADDITIONAL
FEATURES

Figure 1-13 PFD/MFD Controls

The NAV, CRS/BARO, COM, FMS, and ALT knobs are concentric dual knobs, each having small (inner)
and large (outer) control portion. When a portion of the knob is not specified in the text, either may be used.

APPENDICES

Large (Outer) Knob
Small (Inner) Knob

INDEX

Figure 1-14 Dual Concentric Knob

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a
percentage)

NAV Frequency
Transfer Key
3 NAV Knob
Heading Knob

Press to toggle light blue tuning box between NAV1 and NAV2
Turn to manually select a heading

Joystick

Press to display a digital heading momentarily to the left of the Horizontal Situation
Indicator (HSI) and synchronize the Selected Heading to the and current heading
Turn to change map range

CRS/BARO Knob

Press to activate Map Pointer and move in desired direction to pan map
Turn large knob for altimeter barometric pressure setting

AUDIO PANEL
& CNS

Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz)

EIS

Press to toggle Morse code identifier audio on/off
Transfers the standby and active NAV frequencies

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Turn small knob to adjust course (only when HSI is in VOR or OBS Mode)

COM Knob

FLIGHT
MANAGEMENT

Press to re-center the CDI and return course pointer directly to bearing of active
waypoint/station
Turn to tune COM transceiver standby frequencies (large knob for MHz; small for
kHz)
Press to toggle light blue tuning box between COM1 and COM2

COM Frequency
Transfer Key
(EMERG)

HAZARD
AVOIDANCE

The selected COM (green) is controlled with the COM MIC Key (Audio Panel).
Transfers the standby and active COM frequencies

FPL Key

CLR Key
(DFLT MAP)
MENU Key

PROC Key

ENT Key

190-00592-06 Rev. A

Press and hold to display the MFD Navigation Map Page (MFD only).
Displays a context-sensitive list of options for accessing additional features or making
setting changes
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and
approach procedures (IAPs) for a flight plan or selected airport
Validates/confirms selection or data entry

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Erases information, cancels entries, or removes menus

APPENDICES

Direct-to Key (

Press to turn the COM automatic squelch on/off
) Activates the direct-to function and allows the user to enter a destination waypoint
and establish a direct course to the selected destination (specified by identifier,
chosen from the active route)
Displays flight plan information

ADDITIONAL
FEATURES

AFCS

Press and hold two seconds to tune the emergency frequency (121.5 MHz)
automatically into the active frequency field
9 COM VOL/SQ Knob Turn to control COM audio volume level (shown as a percentage in the COM
Frequency Box)

SYSTEM
OVERVIEW

System Overview

FLIGHT
INSTRUMENTS

Press to turn the selection cursor on/off
FMS Knob
(Flight Management Data Entry: With cursor on, turn to enter data in the highlighted field (large
System Knob)
knob moves cursor location; small knob selects character for highlighted cursor
location)

EIS

Scrolling: When a list of information is too long for the window/box, a scroll bar
appears, indicating more items to view. With cursor on, turn large knob to scroll
through the list.
Page Selection: Turn knob on MFD to select the page to view (large knob selects a
page group; small knob selects a specific page from the group)
Press to select softkey shown above the bezel key on the PFD/MFD display

AUDIO PANEL
& CNS

Softkey Selection
Keys
18 ALT Knob

Sets the Selected Altitude, shown above the Altimeter (the large knob selects the
thousands, the small knob selects the hundreds)

Softkey Function

FLIGHT
MANAGEMENT

The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level
or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When
a softkey is selected, its color changes to black text on gray background and remains this way until it is turned
off, at which time it reverts to white text on black background. When a softkey function is disabled, the softkey
label is subdued (dimmed).

HAZARD
AVOIDANCE

Softkeys revert to the previous level after 45 seconds of inactivity.

AFCS

Bezel-Mounted
Softkeys (Press)

Softkey
On

Softkey Names
(Displayed)

Figure 1-15 Softkeys (Second-Level PFD Configuration)

ADDITIONAL
FEATURES

In the following descriptions, top level softkeys are denoted with bullets.

PFD Softkeys

APPENDICES

The CDI, IDENT, TMR/REF, NRST, and ALERTS softkeys undergo a momentary change to black text on
gray background and automatically switch back to white text on black background when selected.

INDEX

The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic,
and lightning (optional). Each softkey sublevel has a BACK Softkey which can be selected to return to the
previous level. The ALERTS Softkey is visible at all softkey levels (label changes if messages are issued).

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

(optional)
INSET

PFD

OBS

CDI

ADF/DME

XPDR

IDENT

TMR/REF

NRST

ALERTS

FLIGHT
INSTRUMENTS

Press the CDI Softkey to cycle through
navigation sources:
- GPS
- NAV1 (VOR/LOC)
- NAV2 (VOR/LOC)

Figure 1-16 Top Level PFD Softkeys

INSET

EIS
AUDIO PANEL
& CNS

Displays Inset Map in PFD lower left corner
• INSET
Removes Inset Map
OFF
(optional) (optional) (optional)
TRAFFIC
OFF
DCLTR
TOPO
TERRAIN STRMSCP NEXRAD XM LTNG
Selects desired amount of map detail; cycles through declutterBACK
levels:ALERTS
DCLTR (3)
DCLTR (No Declutter): All map features visible
Press the OFF or BACK Softkey
TRFC-1
DCLTR-1
DCLTR-1: Removes
land data
to return to the top-level softkeys.
DCLTR-2
TRFC-2
DCLTR-2: Removes
land and SUA data
DCLTR-3
DCLTR-3: Removes everything except active flight plan
TRAFFIC (2) Displays/removes traffic information on Inset Map
PFD
TRFC-1: Displays
traffic on Inset Map.
TRFC-2: Removes everything except traffic. Inset Map position HDG UP only.
Displays/removes topographical data (e.g., coastlines, terrain, rivers, lakes) on Inset Map
TOPO
(optional)
Displays/removes
on Inset
TERRAIN
INSET
PFD terrain
OBS information
CDI
XPDR Map
IDENT TMR/REF
NRST
ALERTS
ADF/DME
(optional)
HSI FMT
BRG1
ALERTS
WIND
BARO Map
BACK(optional)
DFLTS
DME Stormscope
BRG2 information
ALT UNIT
Displays/removes
weather
on STD
Inset
STRMSCP
Press the CDI Softkey to cycle through
Displays/removes NEXRADnavigation
weather
and coverage information on Inset Map (optional)
NEXRAD
sources:
Press the STD BARO or BACK
-Press
GPS the BRG1/BRG2
Displays/removes XM lightning-softkeys
information
on Inset
Mapto return
(optional)
XM LTNG
to display/remove
Softkey
to the top-level
NAV1
(VOR/LOC)

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

INSET

OPTN2

OPTN3

BACK

OFF

ALERTS

ADDITIONAL
FEATURES

OPTN1

AFCS

Bearing
Information
softkeys.
-the
NAV2
(VOR/LOC)
windows and cycle through
bearing sources:
- NAV1/NAV2
- GPS
- ADF

(optional) (optional) (optional)
OFF

TRAFFIC

DCLTR

TOPO

TERRAIN STRMSCP NEXRAD XM LTNG
360 HSI

DCLTR-1

ARC HSI

TRFC-1
TRFC-2

ALERTS
ALERTS

Press the OFF or BACK Softkey
to return to the top-level softkeys.

HPA

BACK

ALERTS

IDENT

BACK

ALERTS

BACK

ALERTS

APPENDICES

DCLTR-2

METERS

BACK
BACK

DCLTR-3
XPDR

Figure 1-17 INSET Softkeys
PFD

ALT

GND

VFR

BRG1

HSI FMT

BRG2

CODE

INDEX

STBY

(optional)
DFLTS

190-00592-06 Rev. A

WIND

DME

ALT UNIT STD BARO

Press the BACK Softkey to
return to the top-level softkeys.

Press the BRG1/BRG2
Press the STD BARO or BACK
softkeys to display/remove Softkey to return to the top-level
6
7
IDENT
BKSP
BACK
ALERTS
the Bearing
Information
softkeys.
windows and cycle through
bearing sources:

2
3
4
5
Garmin
G1000
Pilot’s
Guide
for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
Displays second-level softkeys for additional PFD configuration
Displays the softkeys for enabling or disabling Synthetic Vision features
Displays rectangular boxes representing the horizontal and vertical flight path
of the active flight plan
SYN TERR Enables synthetic terrain depiction
HRZN HDG Displays compass heading along the Zero-Pitch line
APTSIGNS Displays position markers for airports within approximately 15 nm of the
current aircraft position. Airport identifiers are displayed when the airport is
within approximately 9 nm.
Resets PFD to default settings, including changing units to standard
DFLTS
Displays softkeys to select and configure wind data
WIND
Displays wind data in longitudinal and lateral components
OPTN1
Displays wind data total direction and speed
OPTN2
Displays wind data total direction with head and cross-wind speed components
OPTN3
Removes wind information from display
OFF
Displays/removes DME Information Window (optional)
DME
Cycles the Bearing 1 Information Window through:
BRG1
NAV1: Waypoint frequency/identifier and DME information
GPS: Waypoint identifier and GPS distance information
ADF: Waypoint frequency
Off: Removes window
Displays softkeys to select the HSI format
HSI FMT
Displays HSI as a 360° compass rose
360 HSI
Displays HSI as a 140° viewable arc (Bearing Information windows unavailable)
ARC HSI
Cycles the Bearing 2 Information Window through:
BRG2
NAV2: Waypoint frequency/identifier and DME information
GPS: Waypoint identifier and GPS distance information
ADF: Waypoint frequency
Off: Removes window
Displays softkeys for changing the Altimeter barometric setting and altitude displays to
ALT UNIT
metric units
Displays the current and Selected altitudes in meters in addition to feet, when selected
METERS
Displays the Altimeter barometric setting in inches of mercury (in Hg)
IN
Displays the Altimeter barometric setting in hectopascals (hPa)
HPA
Sets barometric pressure to 29.92 in Hg (1013 hPa if metric display is selected)
STD BARO
Selects OBS Mode on the CDI when navigating by GPS (only available with active leg)
• OBS
Cycles CDI through GPS, NAV1 (VOR/LOC), and NAV2 (VOR/LOC) navigation sources
• CDI
• ADF/DME
Displays/removes ADF/DME Radio Tuning Window (optional; may appear as ADF, DME,
or ADF/DME depending on installation)

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

• PFD
SYN VIS
PATHWAY

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

PFD

FLIGHT
INSTRUMENTS

(optional)
SYN VIS

DFLTS

WIND

DME

BRG1

HSI FMT

ALT UNIT STD BARO

BRG2

BACK

ALERTS

OPTN2

OPTN3

OFF

360 HSI

HPA

PATHWAY SYN TERR HRZN HDG APTSIGNS

ALERTS

BACK

ALERTS

BACK

ALERTS

BACK

ALERTS

FLIGHT
MANAGEMENT

METERS

ARC HSI

BACK

AUDIO PANEL
& CNS

OPTN1

EIS

Press the BRG1/BRG2
Press the STD BARO or BACK
softkeys to display/remove Softkey to return to the top-level
the Bearing Information
softkeys.
windows and cycle through
bearing sources:
- NAV1/NAV2
- GPS
- ADF

HAZARD
AVOIDANCE

Figure 1-18 PFD Configuration Softkeys

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

(optional) (optional) (optional)
OFF

SYSTEM
OVERVIEW

System Overview

FLIGHT
INSTRUMENTS

• XPDR
STBY
ON
ALT
GND

AUDIO PANEL
& CNS

EIS

VFR
CODE
0—7
BKSP
• IDENT

FLIGHT
MANAGEMENT

• TMR/REF
• NRST
• ALERTS

DCLTR

TRAFFIC

DCLTR-1

TRFC-1

DCLTR-2

TRFC-2

TOPO

TERRAIN STRMSCP NEXRAD XM LTNG

BACK

ALERTS

Press the OFF or BACK Softkey
to return to the top-level softkeys.

DCLTR-3

Displays transponder mode selection softkeys:
Selects standby mode (Transponder does not reply to any interrogations)
PFD
Selects Mode A (Transponder replies to interrogations)
Selects Mode C – altitude reporting mode (Transponder replies to identification and altitude
interrogations)
Manually selects (optional)
Ground Mode (Transponder does not allow Mode A and Mode C
HSI FMT
BRG1
ALERTS
WIND
BACK
DFLTS
DME
BRG2
ALT UNIT STD BARO
replies, but does permit acquisition squitter and replies to discretely addressed Mode S
interrogations)
Press the BRG1/BRG2
Press the STD BARO or BACK
softkeys to
Automatically enters the VFR code (1200
indisplay/remove
U.S.A. only)Softkey to return to the top-level
the Bearing Information
softkeys.
and cycle
Displays transponder code selectionwindows
softkeys
0-7 through
bearing sources:
Use numbers to enter code
- NAV1/NAV2
- GPS
Removes numbers entered, one at a time
- ADF
Activates theOPTN1
Special
Position
Identification
(SPI) pulse for 18 seconds,
identifying the
BACK
ALERTS
OFF
OPTN2
OPTN3
transponder return on the ATC screen
Displays/removes Timer/References Window
360 HSI ARC HSI
BACK
ALERTS
Displays/removes Nearest Airports Window
Displays/removes Alerts WindowMETERS
IN
HPA
BACK
ALERTS

HAZARD
AVOIDANCE

XPDR

STBY

ALT

GND

VFR

CODE

IDENT

BACK

ALERTS

AFCS

Press the BACK Softkey to
return to the top-level softkeys.

ADDITIONAL
FEATURES

IDENT

BKSP

BACK

ALERTS

Press the IDENT or BACK
Softkey to return to the toplevel softkeys.

INDEX

APPENDICES

Figure 1-19 XPDR Softkeys

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

MFD Softkeys
MFD softkeys vary depending on the page selected. EIS and Navigation Map Page (default MFD page)
softkeys are described here.
MAP

DCLTR

FLIGHT
INSTRUMENTS

ENGINE

SHW CHRT CHKLIST

DCLTR-1
DCLTR-2
DCLTR-3

EIS

LEAN

DEC FUEL INC FUEL RST FUEL

(optional) (optional) (optional)
TERRAIN AIRWAYS STRMSCP NEXRAD XM LTNG

BACK

ENGINE

TRAFFIC

TOPO

AUDIO PANEL
& CNS

Press the ENGINE Softkey to
return to the top-level softkeys.

Press the BACK softkey to
return to the top-level softkeys.

AIRWY ON

FLIGHT
MANAGEMENT

AIRWY LO
AIRWY HI

ENGINE

DONE

EXIT

EMERGCY

HAZARD
AVOIDANCE

The DONE Softkey label changes to UNDO
when the checklist item is already checked.

Figure 1-20 EIS and MFD Softkeys

Displays EIS - Engine Page and second-level engine softkeys; press again to exit page (see the
EIS Section for more information)
Accesses engine leaning assist mode
LEAN
DEC FUEL Decreases displayed fuel remaining in 1-gal increments
INC FUEL Increases displayed fuel remaining in 1-gal increments
RST FUEL Resets displayed fuel remaining to maximum fuel capacity for aircraft and fuel used to zero

• ENGINE

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
Enables second-level Navigation Map Page softkeys
Displays/removes traffic information on Navigation Map Page
Displays/removes topographical data (e.g., coastlines, terrain, rivers, lakes) on Navigation
Map Page
Displays/removes terrain information on Navigation Map Page
TERRAIN
Selects the desired display of Airways; cycles through:
AIRWAYS
AIRWY ON: All Airways displayed
AIRWY LO: Low Altitude (Victor) Airways displayed
AIRWY HI: High Altitude Airways (Jet Routes) displayed
AIRWAYS: Airways are not displayed
STRMSCP Displays/removes Stormscope weather information on Inset Map (optional)
Displays/removes NEXRAD weather/coverage on Navigation Map Page (optional)
NEXRAD
XM LTNG Displays/removes XM lightning information on Navigation Map Page (optional)
Returns to top-level softkeys
BACK
• DCLTR (3) Selects desired amount of map detail; cycles through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Removes land data
DCLTR-2: Removes land and SUA data
DCLTR-3: Removes everything except the active flight plan
• SHW CHRT Displays optional Flite Charts or Chart View charts (optional)
Displays the Checklist Page
• CHKLIST
Selects the highlighted checklist item
DONE
Returns to the top-level softkeys
EXIT
EMERGCY Immediately accesses the emergency procedures

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

• MAP
TRAFFIC
TOPO

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

1.6 Accessing G1000 Functionality
Menus

FLIGHT
INSTRUMENTS

The G1000 has a dedicated MENU Key that when pressed displays a context-sensitive list of options. This
options list allows the user to access additional features or make settings changes which specifically relate to
the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to
additional submenus that are used to view, edit, select, and review options. Menus display ‘No Options’ when
there are no additional features or settings for the window/page selected.

EIS

Navigating a menu:
1) Press the MENU Key to display the menu.

AUDIO PANEL
& CNS

2) Turn the FMS Knob to scroll through a list of available options (a scroll bar always appears to the right of the
window/box when the option list is longer than the window/box).
3) Press the ENT Key to select the desired option.
4) Press the CLR Key or FMS Knob to remove the menu and cancel the operation.
Options for FPL Window

FLIGHT
MANAGEMENT

No Options for
NRST Window

HAZARD
AVOIDANCE

Figure 1-21 Page Menu Examples

AFCS

Data Entry

ADDITIONAL
FEATURES

The FMS Knob can be used for directly entering alphanumeric data (e.g., Flight ID, waypoint identifiers,
barometric minimum descent altitude) into the G1000 In some instances, such as when entering an identifier,
the G1000 tries to predict the desired identifier based on the characters being entered. In this case, if the
desired identifier appears, use the ENT Key to confirm the entry without entering the rest of the identifier
manually. This can save the pilot from having to enter all the characters of the identifier.

APPENDICES

Besides character-by-character data entry, the system also provides a shortcut for entering waypoint identifiers.
When the cursor is on a field awaiting entry of a waypoint identifier, turning the small FMS Knob counterclockwise accesses three different lists of waypoint identifiers for quick selection: flight plan (FPL), nearest
(NRST), and recently-entered (RECENT). The G1000 automatically fills in the identifier, facility, and city fields
with the information for the selected waypoint.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
Using the FMS Knob to enter data:
1) If needed, press the FMS Knob to activate the cursor.

FLIGHT
INSTRUMENTS

2) Use the large FMS Knob to highlight the desired field.
3) Begin entering data.
a) To quickly enter a waypoint identifier, turn the small FMS Knob counter-clockwise to display a list of waypoints
in the active flight plan (list is titled FPL). If desired, turn the small FMS Knob clockwise to scroll through lists
of nearest waypoints (NRST) and recently-entered waypoints (RECENT).

EIS

b) Turn the large FMS Knob to highlight the desired waypoint from the list and press the ENT Key.

Or:
a) Turn the small FMS Knob to select a character for the first placeholder.

AUDIO PANEL
& CNS

Turning the knob clockwise scrolls through the alphabet (where appropriate) toward the letter Z, starting at
K, and the digits zero through nine. Afterwards, turning the knob counter-clockwise scrolls in the opposite
direction.
b) Use the large FMS Knob to move the cursor to the next placeholder in the field.

FLIGHT
MANAGEMENT

c) Repeat, using the small FMS Knob to select a character and the large FMS Knob to move the cursor, until the
field is complete.
d) Press the ENT Key to confirm entry.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

7) Press the FMS Knob or CLR Key to cancel data entry (the field reverts back to its previous information).

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

Page Groups
Note: Refer to other supporting sections in this Pilot’s Guide for details on specific pages.

Active Page Title

EIS

Page Group

FLIGHT
INSTRUMENTS

Information on the MFD is presented on pages which are grouped according to function. The page group and
active page title are displayed in the upper center of the screen, below the Navigation Status Box. In the bottom
right corner of the screen, the current page group, number of pages available in the group, and placement of
the current page within the group are indicated by icons. For some of these pages (Airport/Procedures/Weather
Information, XM, Procedure Loading), the title of the page changes while the page icon remains the same.
MFD

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Page Groups

Pages in Current Group

HAZARD
AVOIDANCE

Selected Page
Figure 1-22 Page Title and Page Group Icons

There are four main page groups, navigated using the FMS Knob; specific pages within each group can vary
depending on the configuration of optional equipment.
AFCS

Selecting a page using the FMS Knob:
1) Turn the large FMS Knob until the desired page group is selected.

ADDITIONAL
FEATURES

2) Turn the small FMS Knob until the desired page is selected.

APPENDICES

There are also several pages (Airport/Procedures/Weather Information and XM pages) which are selected first
from within a main page group with the FMS Knob, then with the appropriate softkey at the bottom of the page
(or from the page menu). In this case, the page remains set to the selected page until a different page softkey is
selected, even if a different page group is selected.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
• Map Page Group (MAP)
Navigation Map

FLIGHT
INSTRUMENTS

Traffic Map
Stormscope (optional)
Weather Data Link (optional)

AUDIO PANEL
& CNS

EIS

Terrain Proximity/TAWS
(TAWS optional)

FLIGHT
MANAGEMENT

Figure 1-23 Map Pages

• Waypoint Page Group (WPT)
Airport/Procedures/Weather Information Pages

HAZARD
AVOIDANCE

- Airport Information
(INFO Softkey)
- Departure Information
(DP Softkey)
- Arrival Information
(STAR Softkey)

AFCS

- Approach Information
(APR Softkey)

ADDITIONAL
FEATURES

- Weather Information (optional)
(WX Softkey)
Intersection Information
NDB Information
VOR Information
Figure 1-24 Waypoint Pages

INDEX

APPENDICES

User Waypoint Information

Airport/
Procedures/
Weather
Information
Pages

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

• Auxiliary Page Group (AUX)
Trip Planning
Utility

FLIGHT
INSTRUMENTS

GPS Status
System Setup
XM Satellite screens (optional)
- XM Information
(INFO Softkey)

EIS

- XM Radio
(RADIO Softkey)

XM
Pages
AUDIO PANEL
& CNS

System Status

Figure 1-25 Auxiliary Pages

FLIGHT
MANAGEMENT

• Nearest Page Group (NRST)
Nearest Airports
Nearest Intersections

HAZARD
AVOIDANCE

Nearest NDB
Nearest VOR
Nearest User Waypoints
Nearest Frequencies

AFCS

Nearest Airspaces

ADDITIONAL
FEATURES
APPENDICES

Figure 1-26 Nearest Pages

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
In addition to the main page groups accessed exclusively using the FMS Knob, there are pages for flight
planning (FPL) and loading procedures (PROC) which are accessed by key. In some instances, softkeys may be
used to access the Procedure Loading pages.

FLIGHT
INSTRUMENTS

The Flight Plan pages are accessed using the FPL Key on the MFD. Main pages within this group are selected
by turning the small FMS Knob.
• Flight Plan Page Group (FPL)
Active Flight Plan
Flight Plan Catalog

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

- Stored Flight Plan
(NEW Softkey)

Figure 1-27 Flight Plan Pages

HAZARD
AVOIDANCE

The Procedure Loading pages may be accessed at any time on the MFD by pressing the PROC Key. A menu
is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading page is
opened. These pages can also be accessed from the Active and Stored Flight Plan pages using the LD softkeys.
Turning the FMS Knob does not scroll through the Procedure Loading pages (note the single page icon in the
lower right corner).
• Procedure Loading Page Group (PROC)

AFCS

Departure Loading
Arrival Loading

APPENDICES

ADDITIONAL
FEATURES

Approach Loading

Figure 1-28 Procedure Loading Pages
INDEX

Information on optional electronic checklist pages is offered later in this section. Checklist pages may be
accessed from any page on the MFD using the CHKLIST Softkey.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

System Settings
G1000 system settings are managed from the System Setup Page. The following settings can be changed:
• Date/time
• Display Units
(see Flight Instruments Section)
• Airspace alerts (see Flight Management Section)
• Arrival alerts (see Flight Management Section)
• MFD Navigation Status Box fields
(see Flight Management Section)

FLIGHT
INSTRUMENTS

• CDI scaling for GPS navigation source
(see Flight Instruments Section)
• COM channel spacing
(see Audio Panel and CNS Section)
• Criteria for displaying nearest airports
(see Flight Management Section)

EIS

• Audio Alerts

Restoring system setup defaults:
AUDIO PANEL
& CNS

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the DFLTS Softkey.
Or:

FLIGHT
MANAGEMENT

a) Press the MENU Key.
b) Highlight ‘Restore Defaults’ and press the ENT Key.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Figure 1-29 System Setup Page

SYSTEM
OVERVIEW

System Overview
Date/Time

FLIGHT
INSTRUMENTS

The G1000 obtains the current Universal Coordinated Time (UTC) date and time directly from the GPS
satellite signals (shown on the AUX - GPS Status Page, Figure 1-11). System time (displayed in the lower
right corner of the PFD) can be displayed in three formats: local 12-hr, local 24-hr, or UTC. Local time is set
by adding/subtracting an offset (hours:minutes) to/from UTC.

AUDIO PANEL
& CNS

EIS

PFD

FLIGHT
MANAGEMENT

Figure 1-30 System Time (Local 24-hr Format)

Configuring the system time:

HAZARD
AVOIDANCE

1) Select the AUX - System Setup Page using the FMS Knob.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the ‘Time Format’ field.
4) Turn the small FMS Knob to select the desired format and press the ENT Key to confirm selection. The ‘Time
Offset’ field is highlighted.

APPENDICES

ADDITIONAL
FEATURES

AFCS

5) Use the FMS Knob to enter the desired time offset (±HH:MM) and press the ENT Key to confirm selection.

INDEX

Figure 1-31 Date/Time Settings (AUX - System Setup Page)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

Display Units
Units in which various quantities are displayed on the G1000 screens are listed on the System Setup Page.
The Navigation Angle reference can be set from here (refer to the Flight Instruments Section).

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

Figure 1-32 Display Unit Settings (AUX - System Setup Page)

N/A

Engine Indication System (EIS)
N/A
N/A

INDEX

HDDD°MM.MM’ All positions
HDDD°MM’SS.S”

Altimeter
Vertical Speed Indicator
VNV altitudes (Active Flight Plan)
Engine Indication System (EIS)

APPENDICES

Pounds

ADDITIONAL
FEATURES

Position

All temperatures on PFD
Total Air Temperature (Trip Planning Page)
Fuel parameters (Trip Planning Page)

Airspeed Indicator
True Airspeed (PFD)
Wind speed vector
Map range (Traffic Page, Terrain
Proximity/TAWS Page)
CDI scaling (System Setup)
Fuel range calculation (EIS)

AFCS

Fuel and
Fuel Flow
Weight

Celsius
Fahrenheit
Gallons

HAZARD
AVOIDANCE

Temperature

Exceptions

FLIGHT
MANAGEMENT

Category
Settings
Affected Quantities
Navigation Angle Magnetic (North) Heading
True (North)
Course
Bearing
Track
Desired Track
Wind direction (Trip Planning Page)
Distance and
Nautical
Crosstrack error (HSI)
Speed
Bearing distances (information windows)
DME distance (information window)
Flight plan distances
Map ranges
DIS, GS, TAS, XTK fields (Navigation Status Box)
All distances on MFD
Altitude buffer distance (System Setup)
Arrival Alert trigger distance (System Setup)
All speeds on MFD
Altitude and
Feet
All altitudes on MFD
Vertical Speed
All elevations on MFD

Table 1-1 Display Units Settings (AUX - System Setup Page)

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview
Pilot Profiles

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

System settings may be saved under a pilot profile. When the system is powered on, the last selected pilot
profile is shown on the MFD Power-up Splash Screen (Figure 1-5). The G1000 can store up to 25 profiles;
the currently active profile, the amount of memory used, and the amount of memory available are shown at
the top of the System Setup Page in the box labeled ‘Pilot Profile’. From here, pilot profiles may be created,
selected, renamed, or deleted.

Figure 1-33 Display Unit Settings (AUX - System Setup Page)

Creating a profile:
AFCS

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
ADDITIONAL
FEATURES

4) Press the ENT Key. A ‘Create Profile’ window is displayed.

5) Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key. Pilot profile names
cannot begin with a blank as the first letter.

APPENDICES

6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile.
Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or current system settings.

INDEX

7) Press the ENT Key.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

8) With ‘CREATE’ highlighted, press the ENT Key to create the profile

Or:

Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the ENT Key to activate the new profile.
FLIGHT
INSTRUMENTS

9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key.
Selecting an active profile:

1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

EIS

3) Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box.
4) Turn the small FMS Knob to display the pilot profile list and highlight the desired profile.
5) Press the ENT Key. The G1000 loads and displays the system settings for the selected profile.

AUDIO PANEL
& CNS

Renaming a profile:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

FLIGHT
MANAGEMENT

3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box.
4) Press the ENT Key.

5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename.

HAZARD
AVOIDANCE

6) Press the ENT Key.

7) Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key.
8) With ‘RENAME’ highlighted, press the ENT Key.
9) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key.

AFCS

Deleting a profile:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

ADDITIONAL
FEATURES

3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box.
4) Press the ENT Key.

5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to delete.

APPENDICES

6) Press the ENT Key.

7) With ‘DELETE’ highlighted, press the ENT Key.
8) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

Timers
The G1000 timers available include:

FLIGHT
INSTRUMENTS

• Stopwatch-like generic timers (available from the PFD Timer/References Window and on the MFD AUX Utility Page)
• Total-time-in-flight timer (MFD AUX - Utility Page)
• Time since departure (MFD AUX - Utility Page)

EIS

The generic timer can be set to count up or down from a specified time (HH:MM:SS). When the countdown
on the timer reaches zero the digits begin to count up from zero. If the timer is reset before reaching zero
on a countdown, the digits are reset to the initial value. If the timer is counting up when reset, the digits are
zeroed.

AUDIO PANEL
& CNS

Setting the generic timer (PFD):
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to select the timer field (hh/mm/ss).

FLIGHT
MANAGEMENT

3) Use the FMS Knob to enter the desired time and press the ENT Key.
4) With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction.
5) Press the ENT Key.
6) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’.

HAZARD
AVOIDANCE

7) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’.
8) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the
digits are reset.
9) To remove the window, press the CLR Key or the TMR/REF Softkey.

APPENDICES

ADDITIONAL
FEATURES

AFCS

PFD

INDEX

Figure 1-34 Generic Timer (Timer/References Window)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

The flight timer can be set to count up from zero starting at system power-up or from the time that the
aircraft lifts off; the timer can also be reset to zero at any time.
Setting the generic timer (MFD AUX - Utility Page):

FLIGHT
INSTRUMENTS

1) Use the FMS Knob to select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

3) Turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key.
4) If a specific starting time is desired:

EIS

a) Use the large FMS Knob to highlight the HH:MM:SS field.
b) Use the FMS Knob to enter the desired time and press the ENT Key.

AUDIO PANEL
& CNS

5) Turn the large FMS Knob to highlight ‘START?’ and press the ENT Key to start the timer. The field changes to
‘STOP?’.
6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’.
7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the
digits are reset.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

Figure 1-35 Timers (AUX - Utility Page)

ADDITIONAL
FEATURES

Setting the flight timer starting criterion:
1) Use the FMS Knob to select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

APPENDICES

3) Turn the large FMS Knob to highlight the field next to the flight timer.
4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key.

Resetting the flight timer:
1) Use the FMS Knob to select the AUX - Utility Page.

INDEX

2) Press the MENU Key.
3) With ‘Reset Flight Timer’ highlighted, press the ENT Key.

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

System Overview

FLIGHT
INSTRUMENTS

The G1000 records the time at which departure occurs, depending on whether the pilot prefers the time
to be recorded from system power-up or from aircraft lift off. The displayed departure time can also be reset
to display the current time at the point of reset. The format in which the time is displayed is controlled
from the System Setup Page.
Setting the departure timer starting criterion:
1) Use the FMS Knob to select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the field next to the departure time.

EIS

4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key.

Resetting the departure time:
AUDIO PANEL
& CNS

1) Use the FMS Knob to select the AUX - Utility Page.
2) Press the MENU Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

3) Use the FMS Knob to highlight ‘Reset Departure Time’ and press the ENT Key.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

System Overview
SYSTEM
OVERVIEW

1.7 Display Backlighting

FLIGHT
INSTRUMENTS

The backlighting of the PFD and MFD displays and bezel and Audio Panel keys can be adjusted automatically or
manually. The default setting (automatic backlighting adjustment) uses photocell technology to automatically adjust
for ambient lighting conditions. Photocell calibration curves are pre-configured to optimize display appearance
through a broad range of cockpit lighting conditions. Manual backlighting adjustment can be accomplished using
the existing instrument panel dimmer bus or the following procedures. In normal operating mode, backlighting
can only be adjusted from the PFD. In Reversionary Mode, it can be adjusted from the remaining display.
Adjusting display backlighting:

EIS

1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’.
2) Turn the small FMS Knob to select ‘MANUAL’.

AUDIO PANEL
& CNS

3) Press the ENT Key. The intensity value is now highlighted.
4) Use the FMS Knob to enter the desired backlighting then press the ENT Key.

5) Turn the large FMS Knob to highlight ‘AUTO’ next to ‘MFD DSPL’ and repeat steps 2-4.

FLIGHT
MANAGEMENT

6) To remove the menu, press the CLR or MENU Key.

Adjusting key backlighting:
1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’.
2) Turn the large FMS Knob to highlight ‘PFD DSPL’.

HAZARD
AVOIDANCE

3) Turn the small FMS Knob in the direction of the green arrowhead to display ‘PFD KEY’.

4) Turn the large FMS Knob to highlight ‘AUTO’.
5) Turn the small FMS Knob to select ‘MANUAL’.
6) Press the ENT Key. The intensity value is now highlighted.

AFCS

7) Use the FMS Knob to enter the desired backlighting and press the ENT Key.

8) Turn the large FMS Knob to highlight ‘MFD DSPL’.
9) Turn the small FMS Knob in the direction of the green arrowhead to display ‘MFD KEY’ and repeat steps 4-7.

ADDITIONAL
FEATURES

10) To remove the menu, press the CLR or MENU Key.
PFD

APPENDICES
INDEX

Figure 1-36 PFD Setup Menu

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

System Overview

Blank Page

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Section 2 Flight Instruments

FLIGHT
INSTRUMENTS

WARNING: If the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup

instruments.
Note: The Automatic Flight Control System (AFCS) provides additional readouts and bugs on selected flight

instruments. Refer to the AFCS Section for details on these bugs and readouts, as they appear on the display
during certain AFCS modes.
EIS
AUDIO PANEL
& CNS

Increased situational awareness is provided by replacing the traditional instruments on the panel with an easyto-scan Primary Flight Display (PFD) that features a large horizon, airspeed, attitude, altitude, vertical speed, and
course deviation information. In addition to the flight instruments, navigation, communication, terrain, traffic,
and weather information are also presented on the PFD and explained in other sections of this Pilot’s Guide.
The following flight instruments and supplemental flight data are displayed on the PFD:
• Airspeed Indicator, showing

• Horizontal Situation Indicator, showing
– Turn Rate Indicator

– True airspeed

– Bearing pointers and information windows

– Airspeed awareness ranges

– Navigation source

– Vspeed reference flags

– Course Deviation Indicator (CDI)
– Bearing pointers and information windows

• Altimeter, showing

– DME Information Window
• Transponder Mode, Code, and Ident/Reply

– Barometric setting

• Course Deviation Indicator (CDI)

– Selected altitude

• Timer/References Window, showing

• Vertical Deviation, Glideslope, and Glidepath
Indicators

– Generic timer

• Vertical Speed Indicator (VSI)

– Barometric minimum descent altitude (MDA)

– Vspeed values
ADDITIONAL
FEATURES

• Vertical Navigation (VNV) indications

AFCS

– Trend vector

HAZARD
AVOIDANCE

• Attitude Indicator with slip/skid indication

FLIGHT
MANAGEMENT

– Indicated airspeed

• Wind data

• Outside air temperature (OAT)

APPENDICES

The PFD also displays various alerts and annunciations.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

FLIGHT
INSTRUMENTS

18
17
16

2
EIS

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

14
3

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

8
1

NAV Frequency Box

Turn Rate Indicator

Airspeed Indicator

Barometric Altimeter Setting

True Airspeed

Vertical Speed Indicator (VSI)

Current Heading

Selected Altitude Bug

Current Track Indicator

Altimeter

Horizontal Situation Indicator ( HSI)

Selected Altitude

Outside Air Temperature (OAT)

COM Frequency Box

Softkeys

Navigation Status Box

System Time

Slip/Skid Indicator

Transponder Data Box

Attitude Indicator

Heading Bug

INDEX

Figure 2-1 Primary Flight Display (Default)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

15
FLIGHT
INSTRUMENTS

EIS

AUDIO PANEL
& CNS

FLIGHT
MANAGEMENT

Flight Plan Window

Selected Heading

Annunciation Window

Vspeed Reference

Selected Course

Wind Data

Vertical Speed Required

Inset Map

Vertical Deviation Indicator

DME Information Window

Current VNV Target Altitude

Bearing Information Windows

AFCS Status Annunciation

Minimum Descent Altitude/
Decision Height

ADDITIONAL
FEATURES

AFCS

Traffic Annunciation

HAZARD
AVOIDANCE

Figure 2-2 Additional PFD Information

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

2.1 Flight Instruments

FLIGHT
INSTRUMENTS

Airspeed Indicator
Note: Refer to the Aircraft Flight Manual Supplement (AFMS) for airspeed criteria and Vspeed values.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

The Airspeed Indicator displays airspeed on a moving tape rolling number gauge. The true airspeed is
displayed in knots below the Airspeed Indicator. The numeric labels and major tick marks on the moving
tape are marked at intervals of 10 knots. The minor tick marks on the moving tape are marked at intervals of
five knots. Speed indication starts at 20 knots, with 60 knots of airspeed viewable at any time. The indicated
airspeed is displayed inside the black pointer. The pointer remains black until reaching never-exceed speed
(VNE), at which point it turns red.

Indicated
Airspeed

Airspeed
Trend
Vector

HAZARD
AVOIDANCE

Speed
Ranges

True
Airspeed

Vspeed
Reference

Figure 2-4 Red Pointer
Showing Overspeed VNE

Figure 2-3 Airspeed Indicator

ADDITIONAL
FEATURES

AFCS

A color-coded (white, green, yellow, and red) speed range strip is located on the moving tape. The colors
denote flaps operating range, normal operating range, caution range, and never-exceed speed (VNE). Red and
yellow ranges are also present for low speed awareness. For EASA-certified aircraft, the yellow low airspeed
awareness band is not shown and the limits on the other lower speed ranges differ (refer to the AFMS for speed
criteria).

INDEX

APPENDICES

The Airspeed Trend Vector is a vertical, magenta line, extending up or down on the airspeed scale, shown
to the right of the color-coded speed range strip. The end of the trend vector corresponds to the predicted
airspeed in 6 seconds if the current rate of acceleration is maintained. If the trend vector crosses VNE, the text
of the actual airspeed readout changes to yellow. The trend vector is absent if the speed remains constant or if
any data needed to calculate airspeed is not available due to a system failure.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Vspeeds (Glide, VR, VX, and VY) can be changed and their flags turned on/off from the Timer/References
Window. When active (on), the Vspeeds are displayed at their respective locations to the right of the airspeed
scale. By default, all Vspeed values are reset and all flags turned off when power is cycled.

FLIGHT
INSTRUMENTS

Changing Vspeeds and turning Vspeed flags on/off:
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the field of the desired Vspeed to be changed.
3) Use the FMS Knob to enter the desired value. When a speed has been changed from a default value, an asterisk
appears next to the speed (Figure 2-5).

EIS

4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field.
5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.

AUDIO PANEL
& CNS

6) To remove the window, press the CLR Key or the TMR/REF Softkey.

FLIGHT
MANAGEMENT

Figure 2-6 Timer/References Menu
HAZARD
AVOIDANCE

Figure 2-5 Timer/References Window

Turning all Vspeed flags on/off:
1) Press the TMR/REF Softkey.

AFCS

2) Press the MENU Key.
3) To activate all Vspeed flags, press the ENT Key with All References On highlighted.
4) To remove all Vspeed flags, turn the FMS Knob to highlight All References Off and press the ENT Key.

ADDITIONAL
FEATURES

Restoring all Vspeed defaults:
1) Press the TMR/REF Softkey.
2) Press the MENU Key.

APPENDICES

3) Turn the FMS Knob to highlight Restore Defaults and press the ENT Key.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

Attitude Indicator

FLIGHT
INSTRUMENTS

Attitude information is displayed over a virtual blue sky and brown ground with a white horizon line. The
Attitude Indicator displays the pitch, roll, and slip/skid information.
9
8

EIS

AUDIO PANEL
& CNS

FLIGHT
MANAGEMENT

Roll Pointer

Roll Scale

Horizon Line

Aircraft Symbol

Land Representation

Pitch Scale

Slip/Skid Indicator

Sky Representation

Roll Scale Zero

Figure 2-7 Attitude Indicator

HAZARD
AVOIDANCE

The horizon line is part of the pitch scale. Above and below the horizon line, major pitch marks and numeric
labels are shown for every 10˚, up to 80˚. Minor pitch marks are shown for intervening 5˚ increments, up to
25˚ below and 45˚ above the horizon line. Between 20˚ below to 20˚ above the horizon line, minor pitch marks
occur every 2.5˚.
The inverted white triangle indicates zero on the roll scale. Major tick marks at 30˚ and 60˚ and minor tick
marks at 10˚, 20˚, and 45˚ are shown to the left and right of the zero. Angle of bank is indicated by the position
of the pointer on the roll scale.

APPENDICES

ADDITIONAL
FEATURES

AFCS

The Slip/Skid Indicator is the bar beneath the roll pointer. The indicator moves with the roll pointer and
moves laterally away from the pointer to indicate lateral acceleration. Slip/skid is indicated by the location of
the bar relative to the pointer. One bar displacement is equal to one ball displacement on a traditional Slip/Skid
Indicator.

INDEX

Figure 2-8 Slip/Skid Indication

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Altimeter

FLIGHT
INSTRUMENTS

The Altimeter displays 600 feet of barometric altitude values at a time on a moving tape rolling number gauge.
Numeric labels and major tick marks are shown at intervals of 100 feet. Minor tick marks are at intervals of 20
feet. The indicated altitude is displayed inside the black pointer.
The Selected Altitude is displayed above the Altimeter in the box indicated by a selection bug symbol. A bug
corresponding to this altitude is shown on the tape. If the Selected Altitude exceeds the range shown on the
tape, the bug appears at the upper or lower edge of the tape. When the metric value is selected it is displayed
in a separate box above the Selected Altitude.

EIS

Setting the Selected Altitude:
T urn the ALT Knob to set the Selected Altitude (large knob for 1000-ft increments, small knob for 100-ft
increments (increments reduce to 10 feet for approach).

If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is also available for the Selected Altitude.
Selected
Altitude

Selected
Altitude
Bug

Barometric
Minimum
Bug

Altimeter Setting (In Hg)

Indicated
Altitude
(Meters)

Barometric
Setting Box
(Hectopascals)
Altimeter Setting (Metric)

AFCS

Barometric
Setting

Selected
Altitude
Bug

HAZARD
AVOIDANCE

Indicated
Altitude

Selected
Altitude
(Meters)

FLIGHT
MANAGEMENT

Altitude
Trend
Vector

AUDIO PANEL
& CNS

ADDITIONAL
FEATURES

Figure 2-9 Altimeter Settings, In Hg and Metric

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments
Altitudes can also be displayed in meters. Note that the altitude tape does not change scale.
Displaying altitude in meters:

FLIGHT
INSTRUMENTS

1) Press the PFD Softkey to display the second-level softkeys.
2) Press the ALT UNIT Softkey.
3) Press the METERS Softkey to turn on metric altitude readouts.
4) Press the BACK Softkey to return to the top-level softkeys.

EIS

When the altitude is displayed in meters, the large and small ALT Knobs adjust the Selected Altitude in 500
meter and 50 meter increments respectively.

AUDIO PANEL
& CNS

A magenta Altitude Trend Vector extends up or down the left of the altitude tape, the end resting at the
approximate altitude to be reached in six seconds at the current vertical speed. The trend vector is not shown
if altitude remains constant or if data needed for calculation is not available due to a system failure.

FLIGHT
MANAGEMENT

The barometric pressure setting is displayed below the Altimeter in inches of mercury (in Hg) or hectopascals
(hPa) when metric units are selected. Adjusting the altimeter barometric pressure setting creates discontinuities
in VNV vertical navigation, moving the descent path. For large adjustments, it may take several minutes for the
aircraft to re-establish on the descent patch. If the change is made while nearing a waypoint with a VNV Target
Altitude, the aircraft may not re-establish on the descent path in time to meet the vertical constraint.
Selecting the altimeter barometric pressure setting:

Turn the BARO Knob to select the desired setting.

HAZARD
AVOIDANCE

Selecting standard barometric pressure (29.92 in Hg):
1) Press the PFD Softkey to display the second-level softkeys.
2) Press the STD BARO Softkey.

AFCS

Changing altimeter barometric pressure setting units:
1) Press the PFD Softkey to display the second-level softkeys.
2) Press the ALT UNIT Softkey.
ADDITIONAL
FEATURES

3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).

Or, press the HPA Softkey to display the barometric pressure setting in hectopascals (hPa).

INDEX

APPENDICES

4) Press the BACK Softkey to return to the top-level softkeys.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

A Baro Transition Alert is provided to alert the pilot to change the barometric pressure setting when crossing
the transition altitude in either direction. This is displayed by the flashing light blue barometric pressure setting
when crossing the transition altitude. The flashing stops when the barometric pressure setting is changed.

FLIGHT
INSTRUMENTS

Setting the Baro Transition Alert:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight Altitude in the Baro Transition Alert box.
4) Turn the small FMS Knob to turn the alert OFF or ON and press the ENT Key.

EIS

5) Turn the small FMS Knob to change the altitude and press the ENT Key.
6) To cancel the selection, press the FMS Knob.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Figure 2-10 Aux - System Setup Page, Baro Transition Alert

Vertical Speed Indicator (VSI)
APPENDICES

The Vertical Speed Indicator (VSI) displays the aircraft vertical speed on a fixed scale with labels at 1000 and
2000 fpm and minor tick marks every 500 fpm. Digits appear in the pointer when the climb or descent rate
is greater than 100 fpm. If the rate of ascent/descent exceeds 2000 fpm, the pointer appears at the edge of the
tape and the rate appears inside the pointer.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

Vertical Deviation
Note: The Glidepath Indicator is only shown for aircraft with GIA 63W Integrated Avionics Units when

FLIGHT
INSTRUMENTS

WAAS is available.

EIS

The Vertical Deviation Indicator (VDI) is a magenta chevron indicating the baro-VNV vertical deviation when
Vertical Navigation (VNV) is being used. The VDI appears in conjunction with the “TOD within 1 minute”
alert. The VDI is removed from the display if vertical deviation becomes invalid. See the Flight Management
Section for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information
about VNV indications on the PFD.

AUDIO PANEL
& CNS

The Glideslope Indicator appears to the left of the Altimeter whenever an ILS frequency is tuned in the
active NAV field. A green diamond acts as the Glideslope Indicator, like a glideslope needle on a conventional
indicator. If a localizer frequency is tuned and there is no glideslope, “NO GS” is heard.

FLIGHT
MANAGEMENT

The glidepath is analogous to the glideslope for GPS approaches supporting WAAS vertical guidance (LNAV+V,
L/VNAV, LPV). When an approach of this type is loaded into the flight plan and GPS is the selected navigation
source, the Glidepath Indicator appears as a magenta diamond during the approach. If the Glidepath Indicator
becomes unavilable past the final approach fix (FAF), “NO GP” is heard.
Full-scale deflection of two dots is 1000 feet.
VNV Target
Altitude

Marker
Beacon
Annunciation

HAZARD
AVOIDANCE

Vertical
Speed
Indicator

AFCS

Vertical
Deviation
Indicator

Glidepath
Indicator

Vertical
Speed
Pointer

ADDITIONAL
FEATURES

Glideslope
Required Indicator
Vertical
Speed

Figure 2-12 Glideslope Indicator

Figure 2-13 Glidepath Indicator

INDEX

APPENDICES

Figure 2-11 Vertical Speed and
Deviation Indicators (VSI and VDI)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Horizontal Situation Indicator (HSI)

FLIGHT
INSTRUMENTS

The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation. Letters
indicate the cardinal points with numeric labels every 30˚. Major tick marks are at 10˚ intervals and minor tick
marks are at 5˚ intervals. A digital reading of the current heading appears on top of the HSI, and the current
track is represented on the HSI by a magenta diamond. The HSI also presents turn rate, course deviation,
bearing, and navigation source information. The HSI is available in two formats, a 360˚ compass rose and a
140˚ arc.
Changing the HSI display format:

EIS

1) Press the PFD Softkey.
2) Press the HSI FRMT Softkey.
3) Press the 360 HSI or ARC HSI Softkey.

AUDIO PANEL
& CNS

The 360˚ HSI contains a Course Deviation Indicator (CDI), with a Course Pointer, To/From Indicator, and a
sliding deviation bar and scale. The course pointer is a single line arrow (GPS, VOR1, and LOC1) or a double
line arrow (VOR2 and LOC2) which points in the direction of the set course. The To/From arrow rotates with
the course pointer and is displayed when the active NAVAID is received.
14

FLIGHT
MANAGEMENT

HAZARD
AVOIDANCE

2
3
12

AFCS

To/From Indicator

Current Track Bug

Course Pointer

Lateral Deviation Scale

Heading Bug

Navigation Source

Flight Phase

Aircraft Symbol

6
7

Course Deviation Indicator
(CDI)
Rotating Compass Rose

Turn Rate/Heading
Trend Vector
14 Current Heading

OBS Mode Active

APPENDICES

Turn Rate Indicator

ADDITIONAL
FEATURES

Lubber Line
INDEX

Figure 2-14 Horizontal Situation Indicator (HSI)

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

FLIGHT
INSTRUMENTS

The Arc HSI is a 140˚ expanded section of the compass rose. The Arc HSI contains a Course Pointer,
combined To/From Indicator and a sliding deviation indicator, and a deviation scale. Upon station passage, the
To/From Indicator flips and points to the tail of the aircraft, just like a conventional To/From flag. Depending
on the navigation source, the CDI on the Arc HSI can appear in two different ways, an arrowhead (GPS, VOR,
OBS) or a diamond (LOC).
Course Pointer

Flight Phase Annunciation

EIS

Navigation
Source

Course
Deviation
and To/From
Indicator

Lateral
Deviation
Scale

AUDIO PANEL
& CNS

Figure 2-15 Arc HSI

FLIGHT
MANAGEMENT

The selected heading is shown to the upper left of the HSI for 3 seconds after being adjusted. The light blue
heading bug on the compass rose corresponds to the selected heading. While the HSI is displayed as an arc, if
the heading bug is adjusted off the shown portion of the compass rose, the digital reading is displayed.
Adjusting the Selected Heading:

Turn the HDG Knob to set the Selected Heading.

Press the HDG Knob to synchronize the bug to the current heading.

HAZARD
AVOIDANCE

The Selected Course is shown to the upper right of the HSI for 3 seconds after being adjusted. While the
HSI is displayed as an arc, the Selected Course is displayed whenever the Course Pointer is not within the 140˚
currently shown.

AFCS

Adjusting the Selected Course:

Turn the CRS Knob to set the Selected Course.

Press the CRS Knob to re-center the CDI and return the course pointer to the bearing of the active waypoint or
navigation station.

ADDITIONAL
FEATURES

Current Track Bug

Current Heading
Selected
Course

APPENDICES

Selected
Heading

Selected
Heading
Bug

INDEX

Figure 2-16 Heading and Course Indications

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Navigation angles (track, heading, course, bearing) are corrected to the computed magnetic variation (Mag
Var) or referenced to true north (T), set on the AUX - System Setup Page. When an approach referenced to
true north has been loaded into the flight plan, the system generates a message to change the navigation angle
setting to True at the appropriate time.

FLIGHT
INSTRUMENTS
EIS

Figure 2-17 Heading and Course Indications (True)

Changing the navigation angle true/magnetic setting:
AUDIO PANEL
& CNS

1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight Nav Angle in the Display Units box.

• TRUE - References angles to true north (T)

• MAGNETIC - Angles corrected to the computed magnetic variation (Mag Var)

FLIGHT
MANAGEMENT

4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Figure 2-18 AUX - System Setup Page, Navigation Angle Settings

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments
Turn Rate Indicator

FLIGHT
INSTRUMENTS

The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right
of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the
current turn rate. The end of the trend vector gives the heading predicted in 6 seconds, based on the present
turn rate. A standard-rate turn is shown on the indicator by the trend vector stopping at the standard turn
rate tick mark, corresponding to a predicted heading of 18˚ from the current heading. At rates greater than 4
deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.

AUDIO PANEL
& CNS

EIS

Half-Standard
Turn Rate
Standard
Turn Rate

Arrow Shown
for Turn Rate
> 4 deg/sec

Figure 2-19 Turn Rate Indicator and Trend Vector

Bearing Pointers and Information Windows

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Two bearing pointers and associated information can be displayed on the HSI for NAV, GPS, and ADF
sources by pressing the PFD Softkey then a BRG or DME Softkey. The bearing pointers are light blue and are
single-line (BRG1) or double-line (BRG2). A pointer symbol is shown in the information windows to indicate
the navigation source. The bearing pointers never override the CDI and are visually separated from the CDI
by a white ring. Bearing pointers may be selected but not necessarily visible due to data unavailability.
Tuning Mode
Frequency

Bearing 1
Pointer

Bearing 2
Pointer

Distance
AFCS

DME Information Window
No
Waypoint
Selected

Station
Identifier

ADDITIONAL
FEATURES

Distance to
Bearing Source

APPENDICES

Bearing
Pointer
Source
Icon
Bearing 1 Information Window

Pointer
Bearing
Icon
Source
Bearing 2 Information Window

INDEX

Figure 2-20 HSI with Bearing and DME Information

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

When a bearing pointer is displayed, the associated information window is also displayed. The Bearing
Information Windows are displayed at the lower sides of the HSI and give the following information:
• Station/waypoint identifier (NAV, GPS)

• Pointer icon (BRG1 = single line, BRG2 = double
line)

• GPS-derived great circle distance to bearing
source

FLIGHT
INSTRUMENTS

• Bearing source (NAV, GPS, ADF)

EIS

• Frequency (ADF)
When the NAV radio is tuned to an ILS frequency the bearing source and the bearing pointer is removed
from the HSI. When NAV1 or NAV2 is the selected bearing source, the frequency is replaced by the station
identifier when the station is within range. If GPS is the bearing source, the active waypoint identifier is
displayed instead of a frequency.

AUDIO PANEL
& CNS

The bearing pointer is removed from the HSI and NO DATA is displayed in the information window if
the NAV radio is not receiving a VOR station or if GPS is the bearing source and an active waypoint is not
selected.
Selecting bearing display and changing sources:
1) Press the PFD Softkey.

FLIGHT
MANAGEMENT

2) Press a BRG Softkey to display the desired bearing pointer and information window with a NAV source.
3) Press the BRG Softkey again to change the bearing source to GPS.
4) To remove the bearing pointer and information window, press the BRG Softkey again.

HAZARD
AVOIDANCE

DME Information Window
The DME Information Window is displayed above the BRG1 Information Window on the 360˚ HSI and in
a box above and along side the Arc HSI. It shows the DME label, tuning mode (NAV1, NAV2, or HOLD),
frequency, and distance. When a signal is invalid, the distance is replaced by –.– – NM Refer to the Audio
Panel and CNS Section for information on tuning the DMEs.

AFCS

Displaying the DME Information Window:
1) Press the PFD Softkey.

ADDITIONAL
FEATURES

2) Press the DME Softkey to display the DME Information Window.
3) To remove the DME Information Window, press the DME Softkey again.

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

Course Deviation Indicator (CDI)
NOTE: During a heading change of greater than 105˚ with respect to the course, the CDI on the Arc HSI

FLIGHT
INSTRUMENTS

switches to the opposite side of the deviation scale and displays reverse sensing.
The Course Deviation Indicator (CDI) moves left or right from the course pointer along a lateral deviation
scale to display aircraft position relative to the course. If the course deviation data is not valid, the CDI is not
displayed.

EIS

360º HSI

AUDIO PANEL
& CNS

Navigation
Source

Scale
Crosstrack
Error

FLIGHT
MANAGEMENT

Arc HSI

Flight
Phase
Navigation
Source

Flight
Phase

Crosstrack
Error
CDI Scale

CDI

CDI
Figure 2-21 Course Deviation Indicator

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

The CDI can display two sources of navigation, GPS or VOR/LOC. The color indicates the current navigation
source, magenta for GPS and green for VOR and LOC. The full scale limits for the CDI are defined by a GPSderived distance when navigating GPS. When navigating using a VOR or localizer (LOC), the CDI uses the
same angular deviation as a mechanical CDI. If the CDI exceeds the maximum deviation on the scale (two dots)
while navigating with GPS, the crosstrack error (XTK) is displayed below the white aircraft symbol.

INDEX

Figure 2-22 Navigation Sources

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Changing navigation sources:
1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the
NAV1 standby frequency in the upper left corner of the PFD.

FLIGHT
INSTRUMENTS

2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning
box over the NAV2 standby frequency.
3) Press the CDI Softkey a third time to return to GPS.
NOTE: KAP 140 equipped aircraft only: Each time the CDI Softkey is pressed or the navigation source

NAV1 Selected for Tuning
and Navigating a VOR

AUDIO PANEL
& CNS

NAV2 Selected for Tuning
and Navigating an ILS

FLIGHT
MANAGEMENT

LOC2
Selected

HAZARD
AVOIDANCE

VOR1
Selected

GPS
Selected

EIS

changes, a message appears (“NAV Source Changed – Select Desired Autopilot Mode”), regardless of
whether or not the autopilot is engaged.

AFCS

Pressing the CDI
Softkey Cycles through
Navigation Sources
Figure 2-23 Selecting a Navigation Source

ADDITIONAL
FEATURES

The system automatically switches from GPS to LOC navigation source and changes the CDI scaling accordingly
when all of the following occur:
• A localizer or ILS approach has been loaded into the active flight plan
• The final approach fix (FAF) is the active waypoint, the FAF is less than 15 nm away, and the aircraft is moving
toward the FAF

APPENDICES

• A valid localizer frequency has been tuned
• The GPS CDI deviation is less than 1.2 times full-scale deflection

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

GPS steering guidance is still provided after the CDI automatically switches to LOC until LOC capture, up
to the Final Approach Fix (FAF) for an ILS approach, or until GPS information becomes invalid. Activating
a Vector-to-Final (VTF; see the Flight Management Section) also causes the CDI to switch to LOC navigation
source; GPS steering guidance is not provided after this switch.

SYSTEM
OVERVIEW

Flight Instruments
GPS CDI Scaling

FLIGHT
INSTRUMENTS

When GPS is the selected navigation source, the flight plan legs are sequenced automatically and
annunciations appear on the HSI for the flight phase. Flight phase annunciations are normally shown in
magenta, but when cautionary conditions exist the color changes to yellow. If the current leg in the flight plan
is a heading leg, HDG LEG is annunciated in magenta beneath the aircraft symbol.

EIS

The current GPS CDI scale setting is displayed as System CDI on the AUX - System Setup Page and the fullscale deflection setting may also be changed (2.0 nm, 1.0 nm, 0.3 nm, or Auto) from this page. If the selected
scaling is smaller than the automatic setting for enroute and terminal phases, the CDI is scaled accordingly
and the selected setting is displayed rather than the flight phase annunciation.
Changing the selected GPS CDI setting:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.

AUDIO PANEL
& CNS

2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight Selected in the GPS CDI box.
4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

5) To cancel the selection, press the FMS Knob or the CLR Key.

Figure 2-24 AUX - System Setup Page, GPS CDI Settings

INDEX

APPENDICES

When set to Auto (default), the GPS CDI scale automatically adjusts to the desired limits based upon the
current phase of flight (Figure 2-25, Table 2-1).

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments

Enroute
(Oceanic if >200 nm
from nearest airport)

Terminal

Approach

0.3 nm

1.0 nm

2.0 nm

0.3 nm

1.0 nm

Terminal

FLIGHT
INSTRUMENTS

CDI Full-scale Deflection

SYSTEM
OVERVIEW

Departure

Refer to accompanying
approach CDI scaling figures

Missed
Approach

EIS
AUDIO PANEL
& CNS

Figure 2-25 Automatic CDI Scaling

• Once a departure procedure is activated, the CDI is scaled for departure (0.3 nm).
• The system switches from departure to terminal CDI scaling (1.0 nm) under the following conditions:

FLIGHT
MANAGEMENT

- The next leg in the procedure is not aligned with the departure runway
- The next leg in the departure procedure is not CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF (see
Glossary for leg type definitions)
- After any leg in the departure procedure that is not CA or FA

HAZARD
AVOIDANCE

• At 30 nm from the departure airport the enroute phase of flight is automatically entered and CDI scaling
changes to 2.0 nm over a distance of 1.0 nm, except under the following conditions:
- When navigating with an active departure procedure, the flight phase and CDI scale does not change
until the aircraft arrives at the last departure waypoint (if more than 30 nm from the departure airport) or
the leg after the last departure waypoint has been activated or a direct-to waypoint is activated.

AFCS

• If after completing the departure procedure the nearest airport is more than 200 nm away from the aircraft
and the approach procedure has not yet commenced, the CDI is scaled for oceanic flight (2.0 nm).

ADDITIONAL
FEATURES

• Within 31 nm of the destination airport (terminal area), the CDI scale gradually ramps down from 2.0 nm
to 1.0 nm over a distance of 1.0 nm, except under the following conditions:
- When navigating with an active arrival route, the flight phase and CDI scale does not change until the
aircraft arrives at the first waypoint in the arrive route (if within 31 nm from the destination airport).

APPENDICES

• During approach, the CDI scale ramps down even further (see Figures 2-26 and 2-27). This transition
normally occurs within 2.0 nm of the final approach fix (FAF). The CDI switches to approach scaling
automatically once the approach procedure is activated or if Vector-to-Final (VTF) is selected.
- If the active waypoint is the FAF, the ground track and the bearing to the FAF must be within 45° of the
final approach segment course.

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

- If the active waypoint is part of the missed approach procedure, the active leg and preceding missed
approach legs must be aligned with the final approach segment course and the aircraft must not have
passed the turn initiation point.

2 nm

FAF

CDI scale varies if VTF is activated

0.3 nm

1.0 nm

2 nm

FAF

Landing
Threshold

CDI scale varies if VTF is activated

Figure 2-26 Typical LNAV and LNAV+V Approach CDI Scaling

EIS

angle based
on database
information

course width

angle set
by system

CDI Full-scale Deflection

0.3 nm

1.0 nm

CDI scale is set to the smaller of 0.3 nm
or an angle set by the system

350 ft

FLIGHT
INSTRUMENTS

CDI Full-scale Deflection

SYSTEM
OVERVIEW

Flight Instruments

Figure 2-27 Typical LNAV/VNAV and LPV Approach CDI Scaling

AUDIO PANEL
& CNS

• When a missed approach is activated, the CDI scale changes to 0.3 nm.
• The system automatically switches back to terminal scaling under the following conditions:
- The next leg in the missed approach procedure is not aligned with the final approach path
- The next leg in the missed approach procedure is not CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

- After any leg in the missed approach procedure that is not CA or FA
Flight Phase
Departure
Terminal
Enroute
Oceanic

Annunciation
DPRT
TERM
ENR
OCN

Approach
(Non-precision)

LNAV

ADDITIONAL
FEATURES

AFCS

Approach
(Non-precision with
Vertical Guidance)
Approach
(LNAV/VNAV)
Approach
(LPV)
Missed Approach

Automatic CDI Full-scale Deflection
0.3 nm
1.0 nm
2.0 nm
2.0 nm

1.0 nm decreasing to 350 feet depending on
variables (see Figure 2-26)
LNAV + V
L/VNAV
LPV
MAPR

1.0 nm decreasing to a specified course width, then
0.3 nm, depending on variables (see Figure 2-27)
0.3 nm

INDEX

APPENDICES

Table 2-1 Automatic GPS CDI Scaling

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

OBS Mode
NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended.

FLIGHT
INSTRUMENTS

Enabling Omni-bearing Selector (OBS) Mode suspends the automatic sequencing of waypoints in a GPS
flight plan (GPS must be the selected navigation source), but retains the current Active-to waypoint as the
navigation reference even after passing the waypoint. OBS is annunciated to the lower right of the aircraft
symbol when OBS Mode is selected.

EIS

While OBS is enabled, a course line is drawn through the Active-to waypoint on the moving map. If
desired, the course to/from the waypoint can now be adjusted. When OBS Mode is disabled, the GPS flight
plan returns to normal operation, with automatic sequencing of waypoints, following the course set in OBS
Mode. The flight plan on the moving map retains the modified course line.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

GPS
Selected
Extended
Course
Line

Pressing the OBS
Softkey Suspends
Waypoint Sequencing

HAZARD
AVOIDANCE

OBS
Mode
Enabled
Pressing the OBS
Softkey Again, Returns
to Normal Operation

AFCS

Figure 2-28 Omni-bearing Selector (OBS) Mode

ADDITIONAL
FEATURES

Enabling/disabling OBS Mode while navigating a GPS flight plan:
1) Press the OBS Softkey to select OBS Mode.
2) Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the
Selected Course with the bearing to the next waypoint.

APPENDICES

3) Press the OBS Softkey again to return to automatic waypoint sequencing.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

EIS

FLIGHT
INSTRUMENTS

As the aircraft crosses the missed approach point (MAP), automatic approach waypoint sequencing is
suspended. SUSP appears on the HSI at the lower right of the aircraft symbol in place of OBS and the OBS
Softkey label changes to SUSP. Pressing the SUSP Softkey resumes automatic sequencing of approach
waypoints.

AUDIO PANEL
& CNS

SUSP
Annunciation

FLIGHT
MANAGEMENT

SUSP Softkey Suspends
Waypoint Sequencing

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Figure 2-29 Suspending Automatic Waypoint Sequencing

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

2.2 Supplemental Flight Data

FLIGHT
INSTRUMENTS

Note: Pressing the DFLTS Softkey turns off metric Altimeter display, the Inset Map and wind data display.

In addition to the flight instruments, the PFD also displays various supplemental information, including
temperatures, wind data, and Vertical Navigation (VNV) indications.

Outside Air Temperature

EIS

The Outside Air Temperature (OAT) is displayed in degrees Celsius (°C) or Fahrenheit (°F) as selected by the
pilot, in the lower left of the PFD under normal display conditions. Temperature is displayed below the true
airspeed in reversionary mode.

AUDIO PANEL
& CNS

Normal Display

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

Reversionary Mode

ADDITIONAL
FEATURES
APPENDICES

Figure 2-30 Outside Air Temperature
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments
Changing temperature display units:
1) Select the AUX - System Setup Page on the MFD using the FMS Knob.

FLIGHT
INSTRUMENTS

2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the TEMP field in the Display Units box.
4) Turn the small FMS Knob to highlight either CELSIUS or FAHRENHEIT and press the ENT Key to confirm the
selection.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

5) To cancel the selection, press the FMS Knob or the CLR Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 2-31 AUX - System Setup Page, Temperature Selection

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Wind Data

Option 2

Option 3

No Data

EIS

Option 1

FLIGHT
INSTRUMENTS

Wind direction and speed in knots can be displayed relative to the aircraft in a window to the upper left of
the HSI. When the window is selected for display, but wind information is invalid or unavailable, the window
displays NO WIND DATA. Wind data can be displayed in three different ways.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 2-32 Wind Data

Displaying wind data:
1) Press the PFD Softkey.

HAZARD
AVOIDANCE

2) Press the WIND Softkey to display wind data below the Selected Heading.
3) Press one of the OPTN softkeys to change how wind data is displayed:
• OPTN 1: Headwind and crosswind components

• OPTN 2: Total wind direction and speed

• OPTN 3: Total wind direction with headwind (H), tailwind (T), and crosswind (X) speed components

AFCS

4) To remove the window, press the OFF Softkey.

ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

Vertical Navigation (VNV) Indications

FLIGHT
INSTRUMENTS

When a VNV flight plan has been activated, VNV indications (VNV Target Altitude, RVSI, VDI) appear on the
PFD in conjunction with the “TOD within 1 minute” message and “Vertical track” voice alert. See the Flight
Management and AFCS sections for details on VNV features. VNV indications are removed from the PFD
according to the criteria listed in the table.
Top of Descent Message

EIS

VNV Target
Altitude

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Vertical
Deviation
Indicator
Required
Vertical
Speed Bug
GPS is
Selected
Navigation
Source

HAZARD
AVOIDANCE

Enroute
Phase of
Flight

Figure 2-33 Vertical Navigation Indications (PFD)

VNV Indication Removed
Required Vertical
Vertical
VNV Target
Speed (RVSI)
Deviation (VDI)
Altitude
Aircraft > 1 min before the next TOD and not on a descent leg
X
X
X
Aircraft > 1 min before the next TOD due to flight plan change
X
X
X
VNV cancelled (CNCL VNV Softkey selected on MFD)
X
X
X
Distance to active waypoint cannot be computed due to
unsupported flight plan leg type (see Flight Management
X
X
X
Section)
Aircraft > 250 feet below active VNV Target Altitude
X
X
X
Current crosstrack or track angle error has exceeded limit
X
X
X
Active altitude-constrained waypoint can not be reached within
X
X
maximum allowed flight path angle and vertical speed
X
Last altitude-constrained waypoint in active flight plan reached
X
X
(30 sec before)

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Criteria

Table 2-2 VNV Indication Removal Criteria

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

2.3 PFD Annunciations and Alerting Functions

FLIGHT
INSTRUMENTS

The following annunciations and alerting functions are displayed on the PFD. Refer to Appendix A for more
information on alerts and annunciations.

System Alerting

EIS

Messages appear in the Alerts Window in the lower right corner of the PFD when a warning, caution, advisory
alert, or G1000 message advisory occurs. System alert messages are provided for awareness of G1000 system
problems or status and may or may not require pilot action. The Alerts Window allows system alerts to be
displayed simultaneously. The FMS Knob is used to scroll through the alert messages. The Alerts Window
is enabled/disabled by pressing the ALERTS Softkey. If the window is already open when a new message is
generated, pressing the ALERTS Softkey to acknowledge the message turns the softkey gray.

AUDIO PANEL
& CNS

The ALERTS Softkey label changes to display the appropriate annunciation when an alert is issued. The
annunciation flashes and the appropriate aural alert sounds until acknowledged by pressing the softkey. The
softkey then reverts to the ALERTS label, and when pressed again opens the Alerts Window to display a
descriptive message of the alert.

FLIGHT
MANAGEMENT

Caution indicates the existence of abnormal conditions on the aircraft that may require pilot intervention. A
flashing CAUTION Softkey annunciation and single aural tone (one chime) indicate the presence of a caution.
The flashing CAUTION Softkey annunciation continues to flash until acknowledged by pressing the CAUTION
Softkey.

HAZARD
AVOIDANCE

Warnings are time-critical and require immediate attention. A flashing WARNING Softkey annunciation and
aural tone (single chime every two seconds) indicate the presence of a warning. The aural tone and flashing
WARNING Softkey annunciation continue until acknowledged by pressing the WARNING Softkey.

AFCS

The Annunciation Window appears to the right of the Vertical Speed Indicator and displays abbreviated
annunciation text for aircraft alerts. Warnings appear in red, cautions in yellow, advisory alerts in white,
and safe operating annunciations in green. New alerts are displayed at the top of the Annunciation Window,
regardless of priority. Once acknowledged, they are sequenced based on priority.
Annunciation
Window

ADDITIONAL
FEATURES

Alerts
Window

APPENDICES

Softkey
Annunciations
INDEX

Figure 2-34 G1000 Alerting System

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

Marker Beacon Annunciations

FLIGHT
INSTRUMENTS

Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude. Outer marker
reception is indicated in blue, middle in yellow, and inner in white. Refer to the Audio Panel and CNS Section
for more information on Marker Beacon Annunciations.
Middle Marker

Inner Marker

EIS

Outer Marker

AUDIO PANEL
& CNS

Altimeter

Figure 2-35 Marker Beacon Annunciations

FLIGHT
MANAGEMENT

Traffic Annunciation
Traffic is displayed symbolically on the PFD Inset Map, the MFD Navigation Map Page, and various other
MFD page maps. Refer to the Hazard Avoidance Section and Appendix F for more details about the Traffic
Information Service (TIS) and optional Traffic Advisory Systems (TAS). When a traffic advisory (TA) is detected,
the following automatically occur:

HAZARD
AVOIDANCE

• The PFD Inset Map is enabled and displays traffic
• A flashing black-on-yellow TRAFFIC annunciation appears to the top left of the Attitude Indicator for five
seconds and remains displayed until no TAs are detected in the area

AFCS

• A single “TRAFFIC” aural alert is heard, unless an optional Traffic Advisory System (TAS) is installed. Refer
to the applicable TAS documentation for alerts generated by TAS equipment.

ADDITIONAL
FEATURES

If additional TAs appear, new aural and visual alerts are generated.

Traffic
Symbols

APPENDICES

PFD Traffic Annunciation

PFD Inset Map with TAS Traffic Displayed

INDEX

Figure 2-36 Traffic Annunciation and Inset Map with Traffic Displayed

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

TAWS Annunciations
Terrain Awareness and Warning System (TAWS) annunciations appear on the PFD at the top left of the Altimeter.
Refer to the Hazard Avoidance Section and Appendix A for information on TAWS alerts and annunciations.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 2-37 Traffic and TAWS Annunciations

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Flight Instruments

Altitude Alerting

FLIGHT
INSTRUMENTS

Altitude Alerting provides the pilot with a visual alert when approaching the Selected Altitude. Whenever the
Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the GFC 700
AFCS, but alerting tones are heard only when the GFC 700 is installed. The following occur when approaching
the Selected Altitude:
• Upon passing through 1000 feet of the Selected Altitude an aural tone is heard. The Selected Altitude changes
to black text on a light blue background and flashes for 5 seconds.

EIS

• When the aircraft passes within 200 feet of the Selected Altitude, the Selected Altitude changes to light blue
text on a black background and flashes for 5 seconds.

AUDIO PANEL
& CNS

• After reaching the Selected Altitude, if the pilot flies outside the deviation band (±200 feet of the Selected
Altitude) an aural tone is heard. The Selected Altitude changes to yellow text on a black background and
flashes for 5 seconds.
Within 1000 ft

Within 200 ft

Deviation of ±200 ft

FLIGHT
MANAGEMENT

Figure 2-38 Altitude Alerting Visual Annunciations

Low Altitude Annunciation

HAZARD
AVOIDANCE

NOTE: A Low Altitude Annunciation is available only when WAAS is available. This annunciation is not

shown for systems equipped with TAWS, unless TAWS is inhibited.

ADDITIONAL
FEATURES

AFCS

When the Final Approach Fix (FAF) is the active waypoint in a GPS WAAS approach using vertical guidance,
a Low Altitude Annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed
altitude at the FAF. A black-on-yellow LOW ALT annunciation appears to the top right of the Altimeter, flashing
for several seconds, then remaining displayed until the condition is resolved.

Altimeter

INDEX

APPENDICES

Figure 2-39 Low Altitude on GPS WAAS Approach

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Minimum Descent Altitude/Decision Height Alerting

FLIGHT
INSTRUMENTS

For altitude awareness, a barometric Minimum Descent Altitude (MDA) or Decision Height (DH) can be set
in the Timer/References Window and is reset when the power is cycled. When active, the altitude setting is
displayed to the bottom left of the Altimeter. Once the altitude is within the range of the tape, a bug appears
at the reference altitude on the Altimeter. The following visual annunciations occur when approaching the
MDA/DH:
• When the aircraft altitude descends to within 2500 feet of the MDA/DH setting, the BARO MIN box appears
with the altitude in light blue text. The bug appears on the altitude tape in light blue once in range.

EIS

• When the aircraft passes through 100 feet of the MDA/DH, the bug and text turn white.
• Once the aircraft reaches MDA/DH, the bug and text turn yellow and the aural alert, “Minimums. Minimums”,
is heard.
White Within 100 ft

Yellow When Altitude Reached

AUDIO PANEL
& CNS

Light Blue Within 2500 ft

FLIGHT
MANAGEMENT

Barometric
Minimum
Bug

HAZARD
AVOIDANCE

Barometric
Minimum
Box

Figure 2-40 Barometric MDA/DH Alerting Visual Annunciations

AFCS

Setting the barometric Minimum Descent Altitude/Decision Height and bug:
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the Minimums field.

ADDITIONAL
FEATURES

3) Turn the small FMS Knob to select BARO. Off is selected by default. Press the ENT Key or turn the large FMS
Knob to highlight the next field.
4) Use the small FMS Knob to enter the desired altitude from zero to 16,000 feet.
5) To remove the window, press the CLR Key or the TMR/REF Softkey.

APPENDICES

Figure 2-41 Barometric MDA/DH

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the MDA.
If the aircraft proceeds to climb after having reached the MDA, once it reaches 50 feet above the MDA, alerting
is disabled.

SYSTEM
OVERVIEW

Flight Instruments

2.4 Abnormal Operations

FLIGHT
INSTRUMENTS

Abnormal GPS Conditions
The annunciations listed in the table can appear on the HSI when abnormal GPS conditions occur. Refer to
the Flight Management Section for more information on Dead Reckoning (DR) Mode.
Annunciation

EIS

LOI

AUDIO PANEL
& CNS

INTEG OK

Location
Lower left of
aircraft symbol
Lower left of
aircraft symbol
Upper right of
aircraft symbol
and PFD Inset
Map

Description
Loss of Integrity Monitoring–GPS integrity is insufficient for the current
phase of flight
Integrity OK–GPS integrity has been restored to within normal limits
(annunciation displayed for 5 seconds)
Dead Reckoning–System is using projected position rather than GPS position
to compute navigation data and sequence active flight plan waypoints

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Table 2-3 Abnormal GPS Conditions Annunciated on HSI

Figure 2-42 Example HSI Annunciations
AFCS

In DR Mode the CDI is removed from the display when GPS is the selected navigation source. In addition, all
GPS-derived data is computed based upon an estimated position and is displayed as yellow text on the display
to denote degraded navigation source information. This data includes the following:

ADDITIONAL
FEATURES

• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
• Wind data and pointers in the Wind Data Box on the PFD

APPENDICES

• Track Indicator
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE values
These items should be verified when operating in Dead Reckoning Mode.

INDEX

Also, while the G1000 is in DR Mode, the autopilot will not couple to GPS, and Terrain Proximity, TERRAINSVS, and TAWS are disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and
waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Flight Instruments
SYSTEM
OVERVIEW

Unusual Attitudes

Nose High

FLIGHT
INSTRUMENTS

When the aircraft enters an unusual pitch attitude, red chevrons pointing toward the horizon warn of extreme
pitch. The chevrons are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon
line.
Nose Low

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 2-43 Pitch Attitude Warnings

• PFD Setup Menu

• AFCS Annunciations

• Windows displayed in the lower
right corner of the PFD:

• Minimum Descent Altitude/
Decision Height readout

• Outside air temperature (OAT)

– Nearest Airports

• Altimeter Barometric Setting

• DME Information Window

– Flight Plan

• Selected Altitude

• Wind data

– Alerts

• VNV Target Altitude

• Transponder Status Box

– Procedures

• System Time

– ADF/DME Tuning

APPENDICES

– Timer/References

ADDITIONAL
FEATURES

• Inset Map

• Vertical Deviation, Glideslope,
and Glidepath Indicators

• Flight director Command Bars

AFCS

• Traffic Annunciations

HAZARD
AVOIDANCE

If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD is removed. The
Altimeter and Airspeed, Attitude, Vertical Speed, and Horizontal Situation indicators remain on the display
and the Bearing Information, Alerts, and Annunciation windows can be displayed during such situations. The
following information is removed from the PFD and their softkeys are disabled when the aircraft experiences
unusual attitudes:

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Flight Instruments

Blank Page

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Engine Indication System
SYSTEM
OVERVIEW

Section 3 Engine Indication System

FLIGHT
INSTRUMENTS

The G1000 Engine Indication System (EIS) displays critical engine, electrical, fuel, and other system parameters
on the left side of the Multi Function Display (MFD) during normal operations (Figure 3-1). EIS information can
be fully expanded to an entire page (EIS - Engine Page) using the ENGINE Softkey. In Reversionary Mode, the
displays are re-configured to present Primary Flight Display (PFD) symbology together with the EIS.

EIS Display
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 3-1 MFD (DA40)

AFCS

Green bands on the instruments indicate normal ranges of operation; yellow and red bands indicate caution
and warning, respectively. White or uncolored bands indicate areas outside of normal operation not yet in the
caution or warning ranges. When unsafe operating conditions occur, the corresponding readouts flash to indicate
cautions and warnings. If sensory data to an instrument becomes invalid or unavailable, a red “X” is displayed
across the instrument.

ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Engine Indication System

3.1 EIS Display
Displays manifold pressure in inches of Mercury (in Hg) to indicate
engine power (DA40 only)

Tachometer (RPM)

AUDIO PANEL
& CNS

Engine Manifold Pressure
Gauge (MAN IN HG)

FLIGHT
MANAGEMENT

FLIGHT
INSTRUMENTS

Fuel Flow Indicator
(FUEL FLOW GPH)
Fuel Pressure Indicator
(FUEL PRESS PSI)
Cylinder Head Temperature
Indicator (CHT)
Oil Temperature Indicator
(OIL TEMP)
Oil Pressure Indicator
(OIL PRES)
Ammeter (AMPS)

Voltmeter (VOLTS)

Displays the primary bus voltage

Fuel Quantity Indicator
(FUEL QTY GAL)

Displays the quantity, in gallons (gal), of fuel in the tanks; pointers labeled
L and R indicate the fuel quantity in each tank

EIS

4
5

HAZARD
AVOIDANCE

Displays propeller speed in revolutions per minute (rpm); the red band
indicates propeller overspeed
Displays current fuel flow in gallons per hour (gph)
Displays the fuel pressure in pounds per square inch (psi) (Option for
EASA certified DA40 aircraft only)
Displays the head temperature of the hottest cylinder (number is shown
in pointer)
Displays engine oil temperature
Displays pressure of oil supplied to the engine
Displays the alternator load in amperes

Standard Tanks: Indicator ranges from 0 to 20 gal with tick marks every 5
gal; only displays to 17 gal per side when full

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Long Range Tanks (optional): Indicator ranges from 0 to 25 gal with tick
marks every 5 gal; only displays to 24 gal per side when full

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Engine Indication System
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

EIS

5
AUDIO PANEL
& CNS

3
6
4

FLIGHT
MANAGEMENT

5
6

7
HAZARD
AVOIDANCE

8
9

10
AFCS

DA40F

DA40

ADDITIONAL
FEATURES

Figure 3-2 EIS Display

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Engine Indication System

3.2 Engine Page

FLIGHT
INSTRUMENTS

Pressing the ENGINE Softkey accesses the EIS - Engine Page, which displays all engine, fuel, fuel calculation,
electrical, and trim information.
ENGINE

LEAN

DEC FUEL INC FUEL RST FUEL

EIS

ENGINE

Figure 3-3 Engine Page Softkeys

AUDIO PANEL
& CNS

ENGINE

FLIGHT
MANAGEMENT

ENGINE
LEAN
DEC FUEL
INC FUEL
RST FUEL

Displays EIS - Engine Page and second-level engine softkeys; press again to exit page
ENGINE
BACK
LEAN
SYSTEM
Accesses Leaning Assist Mode
Decreases displayed fuel remaining in 1-gal increments
Increases
displayed
fuel remaining
1-gal increments
LEAN
SYSTEM
BACK
ENGINE
CYL SLCTinASSIST
Resets displayed fuel remaining to maximum fuel capacity for aircraft and fuel used to zero
Press the ENGINE Softkey to
return to the top-level softkeys.

ENGINE
LEAN
SYSTEM
DEC FUEL INC FUEL RST FUEL
Displays manifold
pressure in inches of Mercury (in BACK
Hg) to indicate engine
Engine Manifold
Pressure
power (DA40 only)
Gauge (MAN IN HG)

Oil Temperature and
Pressure Gauges
(OIL °F PSI)

Displays oil temperature in degrees Fahrenheit (°F) and pressure in pounds
per square inch (psi)

Fuel Quantity Gauges
(L/R FUEL QTY GAL)

Display the amount of fuel in gallons (gal) of fuel in the tanks.

AFCS

HAZARD
AVOIDANCE

Press the BACK Softkey to
return to the top-level softkeys.

Standard Tanks: Indicator ranges from 0 to 20 gal with tick marks every 5
gal; only displays to 17 gal per side when full

ADDITIONAL
FEATURES

Long Range Tanks (optional): Indicator ranges from 0 to 25 gal with tick
marks every 5 gal; only displays to 24 gal per side when full
4

APPENDICES

Electrical Group
(ELECTRICAL)

Displays the alternator load in amperes and the primary bus voltage

INDEX

Displays the total flight hours and is activated when the aircraft becomes
airborne (note that time airborne does not necessarily correspond to
tachometer time)
Fuel Calculations Group Displays calculated fuel used, endurance, and range (in nautical miles,
RANGE NM) based on the displayed fuel remaining and the fuel flow
(FUEL CALCULATOR)
totalizer

Total Time in Service
(TTL TIME IN SVC)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Engine Indication System
Displays exhaust gas (EGT) and head (CHT) temperatures of all cylinders in °F

Fuel Flow and Pressure
Gauge (FUEL GPH PSI)
Fuel pressure option EASA
certified DA40 aircraft only

Displays fuel flow in gallons per hour (gph) and fuel pressure in pounds
per square inch (psi)

Tachometer (RPM)

Displays propeller speed in revolutions per minute (rpm); the red band
indicates propeller overspeed
8

EIS

FLIGHT
INSTRUMENTS

Engine Temperature
Group (TEMPERATURE)

SYSTEM
OVERVIEW

AUDIO PANEL
& CNS

FLIGHT
MANAGEMENT

2
HAZARD
AVOIDANCE

5
3

AFCS

Figure 3-4 Engine Page (DA40)
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Engine Indication System
8

FLIGHT
INSTRUMENTS

AUDIO PANEL
& CNS

EIS

5
3

FLIGHT
MANAGEMENT

Figure 3-5 Engine Page (DA40F)

HAZARD
AVOIDANCE

Fuel Calculations
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time

the fuel was reset.

AFCS

Fuel used (GAL USED), endurance (ENDUR), and range (in nautical miles, RANGE NM) are calculated
based on the displayed fuel remaining (GAL REM) and the fuel flow totalizer. The calculated range also takes
into account the aircraft’s heading and the wind direction and speed. See the Flight Management Section for
information regarding the map feature related to the EIS Fuel Calculations.

ADDITIONAL
FEATURES

Adjusting the fuel totalizer quantity:

On the Engine Page, use the DEC FUEL and INC FUEL softkeys to obtain the desired fuel remaining (GAL REM).

Resetting the fuel totalizer:

APPENDICES

On the Engine Page, press the RST FUEL Softkey; this also resets the fuel remaining (GAL REM) to zero.
Set Fuel
Remaining

INDEX

Calculated
Fuel Used

Calculated
Endurance

Calculated
Range
Figure 3-6 Fuel Calculations Group

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Engine Indication System
SYSTEM
OVERVIEW

3.3 Leaning Assist Mode

FLIGHT
INSTRUMENTS

NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Aircraft
Flight Manual Supplement (AFMS).

A leaning assist function is available on the Engine Page to assist in the leaning process.
Accessing Leaning Assist Mode:
1) Press the ENGINE Softkey to open the Engine Page.

EIS

2) Press the LEAN Softkey to identify peaks.
3) Press the LEAN Softkey again to exit Leaning Assist Mode.

AUDIO PANEL
& CNS

When the LEAN Softkey is pressed, the system initially highlights the number and EGT readout of the cylinder
with the hottest EGT. The ∆ Peak temperature is the difference between the peak temperature and the present
temperature for the peaked cylinder. When the first peak is detected, “1st” is annunciated below that cylinder’s
EGT bar and the temperature is marked in light blue on the graph.

FLIGHT
MANAGEMENT

The system continues to detect peak EGTs for each cylinder lean of peak as the fuel flow is decreased, and the
peak of each cylinder’s EGT is indicated by a light blue marker on the graph. Once all cylinders are lean of peak,
the last cylinder to peak is denoted by the “Last” annunciation below its bar on the graph.

HAZARD
AVOIDANCE

Light Blue Bars
Represent Peaks

Light Blue Bar
Represents Peak

AFCS

Indicates First
Cylinder to Peak

Indicates Last
Cylinder to Peak
ADDITIONAL
FEATURES

Current Difference
from Peak Temperature
(Selected Cylinder)
Figure 3-7 Leaning Assist Mode

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Engine Indication System

3.4 EIS Display in Reversionary Mode

FLIGHT
INSTRUMENTS

In reversionary display mode, the remaining display is re-configured to present PFD symbology together with
the EIS Display (refer to the System Overview for information about display Reversionary Mode).

EIS

When the G1000 displays enter reversionary mode, the EIS is separated into three displays: Engine (identical to
the normal EIS Display on the MFD), Lean, and System. For a description of the Engine Display, refer to Section
3.1. The Lean Display presents temperature information and assistance for engine leaning. The System Display
shows various system parameters and fuel calculations.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS Display

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 3-8 Reversionary Mode (DA40)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

ENGINE

Engine Indication System
LEAN

ENGINE

DEC FUEL INC FUEL RST FUEL

SYSTEM
OVERVIEW

The Engine Display is shown by default. To return to the Engine Display from the Lean or System Display, press
the ENGINE or BACK Softkey.
ENGINE

LEAN

SYSTEM

ENGINE

LEAN

SYSTEM

FLIGHT
INSTRUMENTS

ENGINE

BACK

CYL SLCT ASSIST

EIS

Press the BACK Softkey to
return to the top-level softkeys.

Press the ENGINE Softkey to
return to the top-level softkeys.
ENGINE

LEAN

SYSTEM

DEC FUEL INC FUEL RST FUEL

BACK

AUDIO PANEL
& CNS

Figure 3-9 EIS Softkeys (Reversionary Mode)

Displays second-level engine softkeys
Displays the EIS Lean Display
Cycles through the cylinders to obtain information about a particular cylinder, shown in
light blue on the bar graphs
Accesses Leaning Assist Mode
Displays the EIS System Display
Decreases displayed fuel remaining in 1-gal increments
Increases displayed fuel remaining in 1-gal increments
Resets displayed fuel remaining to maximum fuel capacity for aircraft and fuel used to zero

HAZARD
AVOIDANCE

ASSIST
• SYSTEM
DEC FUEL
INC FUEL
RST FUEL

FLIGHT
MANAGEMENT

• ENGINE
• LEAN
CYL SLCT

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Engine Indication System

Lean Display

FLIGHT
INSTRUMENTS

NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Aircraft
Flight Manual Supplement (AFMS).

The EIS Lean Display provides information and a user interface to perform engine leaning. Exhaust gas
(EGT) and head (CHT) temperatures for each cylinder are displayed in bar graph form with a readout for the
temperature of the selected cylinder shown below each graph.
Accessing the EIS Lean Display:

EIS

1) Press the ENGINE Softkey.
2) Press the LEAN Softkey.

AUDIO PANEL
& CNS

3) To return to the default Engine Display, press the ENGINE or BACK Softkey.

By default, the cylinder with the hottest temperature is selected (number highlighted in light blue) when the
LEAN Softkey is pressed. Bars for cylinders with temperatures in the normal range are shown in white. On the
CHT Bar Graph, caution and warning conditions are indicated in yellow and red, respectively.

FLIGHT
MANAGEMENT

Since only one cylinder’s EGT and CHT are displayed at a time, this information can be cycled through for
each cylinder using the CYL SLCT Softkey; the selected cylinder’s number is highlighted in light blue on the
bar graphs. This softkey is disabled when Leaning Assist Mode is selected.
Monitoring the desired cylinder’s temperatures:

HAZARD
AVOIDANCE

From the Lean Display, press the CYL SLCT Softkey to cycle through each cylinder and view its temperature
information. The selected cylinder number is highlighted in light blue.

AFCS

While in Reversionary Mode, the leaning assist function is available when the ASSIST Softkey is pressed
from the Lean Display to assist in the leaning process (refer to the section on Leaning Assist Mode for more
information).

APPENDICES

ADDITIONAL
FEATURES

Tachometer (RPM)

Fuel Flow (FFLOW GPH)

Exhaust Gas Temperature Exhaust Gas Temperature (EGT) for each cylinder is represented as a bar;
below the graph, the EGT readout is given for the selected cylinder
Bar Graph (EGT °F)
(shown in light blue)

INDEX

Displays manifold pressure in inches of Mercury (in Hg) to indicate engine
power (DA40 only)

Engine Manifold Pressure
Gauge (MAN IN HG)

Displays propeller speed in revolutions per minute (rpm); the red band
indicates propeller overspeed
Displays current fuel flow in gallons per hour (gph)

A hollow block appears to represent the peak EGT for the selected cylinder
when the ASSIST Softkey is pressed
EGT Deviation from Peak Displays the current EGT deviation from peak for the selected cylinder in
degrees Fahrenheit (°F) when the ASSIST Softkey is pressed
(D PEAK)
Cylinder Head Temperature Head temperature for each cylinder is represented as a bar; below the
graph, the CHT readout is given for the selected cylinder (shown in
Bar Graph (CHT °F)
light blue)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Engine Indication System
SYSTEM
OVERVIEW

FLIGHT
INSTRUMENTS

2
EIS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

AFCS

DA40F

DA40

ADDITIONAL
FEATURES

Figure 3-10 Lean Display

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Engine Indication System

System Display

FLIGHT
INSTRUMENTS

NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time
the fuel was reset.

NOTE: Refer to the Aircraft Flight Manual Supplement (AFMS) for limitations.

The EIS System Display shows the dial gauges, various system parameters, and fuel calculations. Fuel
calculations are based on the displayed fuel remaining (GAL REM) and the fuel flow totalizer.

EIS

Accessing the EIS System Display:
1) Press the ENGINE Softkey.

AUDIO PANEL
& CNS

2) Press the SYSTEM Softkey.
3) To return to the default Engine Display, press the ENGINE or BACK Softkey.

Adjusting the fuel totalizer quantity:

FLIGHT
MANAGEMENT

From the System Display, press the DEC FUEL or INC FUEL Softkey to adjust the fuel remaining (GAL REM).

Resetting the fuel totalizer:
From the System Display, press the RST FUEL Softkey. This also resets the fuel remaining (GAL REM) to zero.
1 Engine Manifold Pressure Gauge Displays manifold pressure in inches of Mercury (in Hg) to indicate
engine power (DA40 only)
(MAN IN HG)
2
Shows propeller speed in revolutions per minute (rpm); the red band
Tachometer (RPM)
indicates propeller overspeed
3
Engine oil temperature is shown in degrees Fahrenheit (°F)
Oil Temperature (OIL °F)

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Oil Pressure (OIL PSI)

Voltmeter (VOLTS)

Pressure of oil supplied to the engine is displayed in pounds per square
inch (psi)
Shows the primary bus voltage

Ammeter (AMPS)

Shows the alternator load in amperes

Fuel Flow (FFLOW GPH)

Displays current fuel flow in gallons per hour (gph)

Fuel Pressure (FPRESS PSI)

Fuel Remaining (GAL REM)

Fuel Used (GAL USED)

Displays the fuel pressure in pounds per square inch (psi) (Option for
EASA certified DA40 aircraft only)
Current fuel remaining in gallons as set by the pilot and adjusted for
fuel burn since last set
Quantity of fuel used in gallons

Endurance (ENDUR)

Range (RANGE NM)

Total Time in Service (TTL
TIME IN SVC)

Flight time remaining with fuel onboard (HH:MM when more than an
hour remains)
Aircraft range in nautical miles
Displays the total flight hours and is activated when the aircraft becomes
airborne (note that time airborne does not necessarily correspond to
tachometer time)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Engine Indication System
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

EIS

4
5
7
8

10
11
12

5
6
7

9
10
11
12

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

DA40

DA40F
ADDITIONAL
FEATURES

Figure 3-11 System Display

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Engine Indication System

Blank Page

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

Section 4 audio panel and CNS

FLIGHT
INSTRUMENTS

4.1 Overview
The Communication/Navigation/Surveillance (CNS) system includes the Audio Panel, communication radios,
navigation radios, and Mode S transponder. The System Overview Section provides a block diagram description
of the Audio Panel and CNS system interconnection.
CNS operation in Diamond DA40/40F aircraft is performed by the following Line Replaceable Units (LRUs):
• Audio Panel

• Multifunction Display (MFD)

• Mode S Transponder

EIS

• Primary Flight Display (PFD)

AUDIO PANEL
& CNS

• Integrated Avionics Unit (2)
The MFD/PFD controls are used to tune the communication transceivers and navigation radios.

FLIGHT
MANAGEMENT

The Audio Panel provides the traditional audio selector functions of microphone and receiver audio selection.
The Audio Panel includes an intercom system (ICS) between the pilot, copilot, and passengers, a marker beacon
receiver, and a COM clearance recorder. Ambient noise from the aircraft radios is reduced by a feature called
Master Avionics Squelch (MASQ). When no audio is detected, MASQ processing further reduces the amount of
background noise from the radios.

HAZARD
AVOIDANCE

The Mode S transponder is controlled with softkeys and the FMS Knob located on the Primary Flight Display
(PFD). The Transponder Data Box is located to the left of the System Time Box. The data box displays the active
four-digit code, mode, and reply status (Figure 4-1).

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Audio Panel and CNS

MFD/PFD Controls and Frequency Display
2

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

9
10

HAZARD
AVOIDANCE

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-1 MFD/PFD Controls, COM/NAV Frequency Tuning Boxes, and ADF/DME Tuning Window (PFD Shown)

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS

COM Frequency Box – Displays COM standby and active frequency fields and volume. The selected COM
transceiver frequency is displayed in green.

COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for
kHz). Press to move the tuning box (light blue box) and Frequency Transfer Arrow between COM1 and
COM2.

COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Press and hold this key
for two seconds to tune the emergency frequency (121.500 MHz) automatically into the active frequency
field.

COM VOL/SQ Knob – Controls COM audio volume level. Press to turn the COM automatic squelch on
and off. Volume level is shown in the COM frequency field as a percentage.

ADF/DME Tuning Window – Displays ADF frequencies, volume setting, and modes, and DME tuning
selection. Display by pressing the ADF/DME Softkey.

ENT Key – Validates or confirms an ADF frequency or ADF/DME mode and Auto-tune selection.

FMS Knob – Flight Management System Knob, used to enter transponder codes, enter ADF frequencies,
select ADF/DME modes, and Auto-tune entries when ADF/DME Tuning Window or NRST Window is
present. Press the FMS Knob to turn the selection cursor on and off. The large knob moves the cursor in
the window. The small knob selects individual characters for the highlighted cursor location.

Transponder Data Box – Indicates the selected transponder code, operating mode, reply, and ident status
for the transponder.

ADDITIONAL
FEATURES

NAV Frequency Box – Displays NAV standby and active frequency fields, volume, and station ID. The
frequency of the NAV radio selected for navigation is displayed in green.

AFCS

HAZARD
AVOIDANCE

NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz).
Press to move the tuning box (light blue box) and Frequency Transfer Arrow between NAV1 and NAV2.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies.

EIS

FLIGHT
INSTRUMENTS

NAV VOL/ID Knob – Controls NAV audio volume level. Press to turn the Morse code identifier audio on
and off. Volume level is shown in the NAV frequency field as a percentage.

SYSTEM
OVERVIEW

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Audio Panel and CNS

12
14

AUDIO PANEL
& CNS

FLIGHT
MANAGEMENT

HAZARD
AVOIDANCE

EIS

FLIGHT
INSTRUMENTS

Audio Panel Controls

AFCS

Figure 4-2 Audio Panel Controls

INDEX

APPENDICES

ADDITIONAL
FEATURES

NOTE: When a key is selected, a triangular annunciator above the key is illuminated.

COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when
this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receive can be
added by pressing the COM2 Key.

COM1 – When selected, audio from the #1 COM receiver can be heard.

COM2 MIC – Selects the #2 transmitter for transmitting. COM2 receive is simultaneously selected when
this key is pressed allowing received audio from the #2 COM receiver to be heard. COM1 receive can be
added by pressing the COM1 Key.

COM2 – When selected, audio from the #2 COM receiver can be heard.

COM3 MIC – Not used in DA40/40F aircraft.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS

SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the
speaker.

MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver
audio. Unmutes automatically when new marker beacon audio is received. Also, stops play of recorded
COM audio.

HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity.

DME – Turns optional DME audio on or off.

NAV1 – When selected, audio from the #1 NAV receiver can be heard.

ADF – Turns optional ADF receiver audio on or off.

NAV2 – When selected, audio from the #2 NAV receiver can be heard.

AUX – Not used in DA40/40F aircraft.

MAN SQ – Enables manual squelch for the intercom. When the intercom is active, press the PILOT Knob
to illuminate SQ. Turn the PILOT/PASS Knobs to adjust squelch.

PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the
previous block of recorded audio is played. Each subsequent press plays each previously recorded block.
Pressing the MKR/MUTE Key during play of a memory block stops play.

PILOT – Selects and deselects the pilot intercom isolation.

COPLT – Selects and deselects the copilot intercom isolation.

PILOT Knob – Press to switch between volume and squelch control as indicated by illumination of VOL
or SQ. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch
adjustment.

PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be
selected to allow squelch adjustment.

DISPLAY BACKUP Button – Manually selects Reversionary Mode.

APPENDICES

ADDITIONAL
FEATURES

PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key
is pressed.

AFCS

HAZARD
AVOIDANCE

TEL – Not used in DA40/40F aircraft.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

COM 1/2 – Not used in DA40/40F aircraft.

EIS

FLIGHT
INSTRUMENTS

COM3 – Not used in DA40/40F aircraft.

SYSTEM
OVERVIEW

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Audio Panel and CNS

4.2 COM Operation

FLIGHT
INSTRUMENTS

COM Transceiver Selection and Activation
NOTE: During PA Mode, the COM MIC Annunciator is extinguished and the COM active frequency color

changes to white, indicating that neither COM transmitter is active.
NOTE: When turning on the G1000 for use, the system remembers the last frequencies used and the active

EIS

COM transceiver state prior to shutdown.

AUDIO PANEL
& CNS

The COM Frequency Box is composed of four fields; the two active frequencies are on the left side and the
two standby frequencies are on the right. The COM transceiver is selected for transmitting by pressing the
COM MIC Keys on the Audio Panel. During reception of audio from the COM radio selected for transmission,
audio from the other COM radio is muted.

FLIGHT
MANAGEMENT

An active COM frequency displayed in green indicates that the COM transceiver is selected on the Audio
Panel (COM1 MIC or COM2 MIC Key). Both active COM frequencies appearing in white indicate that no COM
radio is selected for transmitting (PA Key is selected on the Audio Panel).
Frequencies in the standby field are displayed in either white or gray. The standby frequency in the tuning
box is white. The other standby frequency is gray.

HAZARD
AVOIDANCE

Active
Fields

Standby
Fields
Top Section of
the Audio Panel

AFCS

Tuning Box

ADDITIONAL
FEATURES

COM2 Radio is Selected
on the Audio Panel

INDEX

APPENDICES

Figure 4-3 Selecting a COM Radio for Transmit

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

Transmit/Receive Indications

FLIGHT
INSTRUMENTS

During COM transmission, a white TX appears by the active COM frequency replacing the Frequency
Transfer Arrow. On the Audio Panel, when the active COM is transmitting, the active transceiver COM MIC
Key Annunciator flashes approximately once per second.
During COM signal reception, a white RX appears by the active COM frequency replacing the Frequency
Transfer Arrow. Entertainment audio, if selected, is muted during active COM radio reception. Refer to
Additional Audio Panel Functions later in this section, and details on the Data Link Receiver in the Additional
Features Section.

EIS
AUDIO PANEL
& CNS

Transmit and
Receive Indicators

Annunciator
Flashes During
Transmission

Figure 4-4 COM Radio Transmit and Receive Indications

FLIGHT
MANAGEMENT

COM Transceiver Manual Tuning
The COM frequency controls and frequency boxes are on the right side of the MFD and PFD.
Manually tuning a COM frequency:

HAZARD
AVOIDANCE

1) Turn the COM Knob to tune the desired frequency in the COM Tuning Box (large knob for MHz; small knob for
kHz).
2) Press the Frequency Transfer Key to transfer the frequency to the active field.
3) Adjust the volume level with the COM VOL/SQ Knob.
4) Press the COM VOL/SQ Knob to turn automatic squelch on and off.

AFCS

Turn the VOL/SQ Knob to adjust
volume. Press the Knob to Turn
Automatic Squelch On or Off

ADDITIONAL
FEATURES

Press the Frequency Transfer
Key to Transfer COM
Frequencies Between Active
and Standby Frequency Boxes
Turn the COM Knob to
Tune the Frequency in
the Tuning Box

APPENDICES

Figure 4-5 COM Frequency Tuning

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Audio Panel and CNS
Selecting the Radio to be Tuned

FLIGHT
INSTRUMENTS

Press the small COM Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the
upper and lower radio frequency fields.

EIS

Press the COM Knob to
Switch the Tuning Box From
One COM Radio to the Other

AUDIO PANEL
& CNS

Figure 4-6 Switching COM Tuning Boxes

Quick-Tuning and Activating 121.500 MHz

FLIGHT
MANAGEMENT

Pressing and holding the COM Frequency Transfer Key for two seconds automatically loads the emergency
COM frequency (121.500 MHz) in the active field of the COM radio selected for tuning (the one with the
transfer arrow). In the example shown, pressing the Audio Panel COM2 MIC Key activates the transceiver.

HAZARD
AVOIDANCE

Press for Two Seconds to
Load 121.500 MHz

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-7 Quickly Tuning 121.500 MHz

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

Auto-Tuning the COM Frequency
COM frequencies can be automatically tuned from the following:
• Nearest Airports Window (PFD)
• NRST – Nearest Frequencies Page (ARTCC, FSS, WX)

FLIGHT
INSTRUMENTS

• WPT – Airport Information Page

• NRST – Nearest Airspaces Page

• NRST – Nearest Airports Page

Auto-Tuning from the PFD

EIS

COM frequencies for the nearest airports can be automatically tuned from the Nearest Airports Window on
the PFD. When the desired frequency is entered, it becomes a standby frequency. Pressing the Frequency
Transfer Key places this frequency into the COM Active Frequency Field.

AUDIO PANEL
& CNS

Auto-tuning a COM frequency for a nearby airport from the PFD:
1) Press the NRST Softkey on the PFD to open the Nearest Airports Window. A list of 25 nearest airport identifiers
and COM frequencies is displayed.
2) Turn the FMS Knob to scroll through the list and highlight the desired COM frequency.

FLIGHT
MANAGEMENT

3) Press the ENT Key to load the COM frequency into the COM Standby Tuning Box.
4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Press the NRST
Softkey to Open
the Nearest
Airports Window
Figure 4-8 Nearest Airports Window (PFD)

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

SYSTEM
OVERVIEW

Audio Panel and CNS
Auto-Tuning from the MFD

FLIGHT
INSTRUMENTS

Frequencies can be automatically loaded into the COM Frequency Box from pages in the NRST or WPT
page group by highlighting the frequency and pressing the ENT Key (Figures 4-9, 4-10, and 4-11).
Auto-tuning a COM frequency from the WPT and NRST Pages:
1) From any page that the COM frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or the
appropriate softkey.
2) Turn the FMS Knob to place the cursor on the desired COM frequency (Figure 4-11).

EIS

3) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio.

AUDIO PANEL
& CNS

4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field.
Press the ENT Key to
Load a Highlighted
Frequency into
the COM Standby
Frequency Box

FLIGHT
MANAGEMENT

Turn the FMS
Knob to Scroll
Through a List
of Frequencies

Figure 4-9 Frequency Auto-Tuning from the MFD

HAZARD
AVOIDANCE

Or:

1) Press the MENU Key to display the page menu.
2) Turn the large FMS Knob to scroll through the menu options.
3) Press the ENT Key to place the cursor on the desired selection.

AFCS

4) Scroll through the frequency selections with the FMS Knob or the ENT Key.
5) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio.

INDEX

APPENDICES

ADDITIONAL
FEATURES

6) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field.

Nearest Airports Menu

Nearest Frequencies Menu

Nearest Airspaces Menu

Figure 4-10 Nearest Pages Menus

100

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

On the WPT - Airport Information Page, the cursor can be placed on the frequency field by pressing the
FMS Knob and scrolling through the list. The frequency is transferred to the COM Standby Field with the
ENT Key.

Selected Airport
Identifier and
Information

FLIGHT
INSTRUMENTS

Press Frequency
Transfer Key to Load
Frequency into COM
Active Frequency Field

EIS
AUDIO PANEL
& CNS

Runway
Information

HAZARD
AVOIDANCE

Figure 4-11 WPT – Airport Information Page

Press INFO Softkey for
AIRPORT, RUNWAYS,
and FREQUENCIES
Windows

FLIGHT
MANAGEMENT

Press ENT Key to Load
Frequency into COM
Standby Field. Cursor
then Advances to
Next Frequency.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

101

SYSTEM
OVERVIEW

Audio Panel and CNS

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

COM frequencies can also be auto-tuned from the NRST – Nearest Airspaces, NRST – Nearest Frequencies,
and NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU
Key, the FMS Knob, and the ENT Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 4-12 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages

102

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

Frequency Spacing

FLIGHT
INSTRUMENTS

The G1000 COM radios can tune either 25-kHz spacing (118.000 to 136.975 MHz) or 8.33-kHz spacing
(118.000 to 136.990 MHz) for 760-channel or 3040-channel configuration. When 8.33-kHz channel spacing
is selected, all of the 25-kHz channel spacing frequencies are also available in the complete 3040-channel list.
COM channel spacing is set on the System Setup Page of the AUX Page Group.

25-kHz Channel
Spacing

EIS

8.33-kHz Channel
Spacing
Figure 4-13 COM Channel Spacing

AUDIO PANEL
& CNS

Changing COM frequency channel spacing:
1) Select the AUX – System Setup Page.
2) Press the FMS Knob to activate the flashing cursor.

FLIGHT
MANAGEMENT

3) Turn the large FMS Knob to highlight the Channel Spacing Field in the COM Configuration Box.
4) Turn the small FMS Knob to select the desired channel spacing.
5) Press the ENT Key to complete the channel spacing selection.

While the COM CONFIG Window is selected, the G1000 softkeys are blank.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Select 8.33-kHz
or 25.0-kHz
COM Frequency
Channel Spacing
AUX - SYSTEM
SETUP PAGE

INDEX

Figure 4-14 AUX – System Setup Page

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

103

SYSTEM
OVERVIEW

Audio Panel and CNS

Automatic Squelch

FLIGHT
INSTRUMENTS

Automatic Squelch quiets unwanted static noise when no audio signal is received, while still providing good
sensitivity to weak COM signals. To disable Automatic Squelch, press the VOL/SQ Knob. When Automatic
Squelch is disabled, COM audio reception is always on. Continuous static noise is heard over the headsets and
speaker, if selected. Pressing the VOL/SQ Knob again enables Automatic Squelch.

EIS

When Automatic Squelch is disabled, a white SQ appears next to the COM frequency.

Squelch
Indication

Press the COM VOL/
SQ Knob to turn off
Automatic Squelch.
Press again to restore
Automatic Squelch.

AUDIO PANEL
& CNS

Figure 4-15 Overriding Automatic Squelch

Volume

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

COM radio volume level can be adjusted from 0 to 100% using the VOL/SQ Knob. Turning the knob
clockwise increases volume, turning the knob counterclockwise decreases volume. When adjusting volume,
the level is displayed in place of the standby frequencies. Volume level indication remains for two seconds after
the change.

COM Volume
Level Remains for
Two Seconds

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-16 COM Volume Level

104

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

4.3 NAV Operation
NAV Radio Selection and Activation

FLIGHT
INSTRUMENTS

The NAV Frequency Box is composed of four fields; two standby fields and two active fields. The active
frequencies are on the right side and the standby frequencies are on the left.

EIS

A NAV radio is selected for navigation by pressing the CDI Softkey located on the PFD. The active NAV
frequency selected for navigation is displayed in green. Pressing the CDI Softkey once selects NAV1 as the
navigation radio. Pressing the CDI Softkey a second time selects NAV2 as the navigation radio. Pressing the
CDI Softkey a third time activates GPS mode. Pressing the CDI Softkey again cycles back to NAV1.
While cycling through the CDI Softkey selections, the NAV Tuning Box and the Frequency Transfer Arrow are
placed in the active NAV Frequency Field and the active NAV frequency color changes to green.

AUDIO PANEL
& CNS

The three navigation modes that can be cycled through are:
• VOR1 (or LOC1) – If NAV1 is selected, a green single line arrow (not shown) labeled either VOR1 or LOC1
is displayed on the HSI and the active NAV1 frequency is displayed in green.

FLIGHT
MANAGEMENT

• VOR2 (or LOC2) – If NAV2 is selected, a green double line arrow (shown) labeled either VOR2 or LOC2 is
displayed on the HSI and the active NAV2 frequency is displayed in green.
• GPS – If GPS Mode is selected, a magenta single line arrow (not shown) appears on the HSI and neither NAV
radio is selected. Both active NAV frequencies are then displayed in white.
Active
Fields

HAZARD
AVOIDANCE

Standby
Fields

Tuning Box
AFCS

The NAV Radio is
Selected by Pressing
the CDI Softkey

ADDITIONAL
FEATURES

Figure 4-17 Selecting a NAV Radio for Navigation

APPENDICES

See the Flight Instruments Section for selecting the DME and Bearing Information windows and using VOR
or ADF as the source for the bearing pointer.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

105

SYSTEM
OVERVIEW

Audio Panel and CNS

EIS

FLIGHT
INSTRUMENTS

NAV radios are selected for listening by pressing the corresponding keys on the Audio Panel. Pressing the
NAV1, NAV2, ADF, or DME Key selects and deselects the navigation radio source. Selected audio can be heard over
the headset and the speaker (if selected). All radios can be selected individually or simultaneously.

AUDIO PANEL
& CNS

Figure 4-18 Selecting a NAV Radio Receiver

NAV Receiver Manual Tuning
The NAV frequency controls and frequency boxes are on the left side of the MFD and PFD.

FLIGHT
MANAGEMENT

Manually tuning a NAV frequency:
1) Turn the NAV Knob to tune the desired frequency in the NAV Tuning Box.
2) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field.
3) Adjust the volume level with the NAV VOL/ID Knob.

HAZARD
AVOIDANCE

4) Press the NAV VOL/ID Knob to turn the Morse code identifier audio on and off.

AFCS

Turn VOL/ID Knob to adjust
volume. Press Knob to Turn
Morse Code On or Off.
Press the Frequency Transfer Key to
Transfer NAV Frequencies Between
Active and Standby Frequency Fields

ADDITIONAL
FEATURES

Turn the NAV Knob to
Tune the Frequency in
the Tuning Box

INDEX

APPENDICES

Figure 4-19 NAV Frequency Tuning

106

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Audio Panel and CNS
SYSTEM
OVERVIEW

Selecting the Radio to be Tuned
Press the small NAV Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the
upper and lower radio frequency fields.

FLIGHT
INSTRUMENTS

Press the NAV Knob to
Switch the Tuning Box From
One NAV Radio to the Other

EIS

Figure 4-20 Switching NAV Tuning Boxes
AUDIO PANEL
& CNS

VOR/LOC ID
When the Morse code Identifier audio is on for a NAV radio, a white ID appears to the left of the active
NAV frequency.

HAZARD
AVOIDANCE

The Morse Code Identifier
for the GHM VOR is On

FLIGHT
MANAGEMENT

In the example shown, in order to listen to either station identifier, press the NAV1 or NAV2 Key on the
Audio Panel. Pressing the VOL/ID Knob turns off the Morse code audio only in the radio with the NAV
Tuning Box. To turn off both NAV IDs, transfer the NAV Tuning Box between NAV1 and NAV2 with the small
NAV Knob and press the VOL/ID Knob again to turn the Morse code off in the other radio.

Station
Identifier
Figure 4-21 NAV Radio ID Indication

AFCS

Volume

ADDITIONAL
FEATURES

NAV Radio volume level can be adjusted from 0 to 100% using the VOL/ID Knob. Turning the knob
clockwise increases volume, counterclockwise decreases volume.
When adjusting, the level is displayed in place of the standby frequencies. Volume level indication remains
for two seconds after the change.

APPENDICES

NAV Volume
Level Remains
for Two Seconds

Figure 4-22 NAV Volume Levels

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

107

SYSTEM
OVERVIEW

Auto-Tuning a NAV Frequency from the MFD

FLIGHT
INSTRUMENTS

Audio Panel and CNS

• WPT – VOR Information

• NRST – Nearest Frequencies (FSS, WX)

• NRST – Nearest Airports

• NRST – Nearest Airspaces

NAV frequencies can be selected and loaded from the following MFD pages:
• WPT – Airport Information
• NRST – Nearest VOR

EIS

The MFD provides auto-tuning of NAV frequencies from waypoint and nearest pages. During enroute
navigation, the NAV frequency is entered automatically into the NAV standby frequency field. During approach
activation the NAV frequency is entered automatically into the NAV active frequency field.
Frequencies can be automatically loaded into the NAV Frequency Box from pages in the NRST or WPT page
group by highlighting the frequency and pressing the ENT Key (Figures 4-23, 4-24, and 4-25).

AUDIO PANEL
& CNS

Auto-tuning a NAV frequency from the WPT and NRST Pages:
1) From any page that the NAV frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or the
appropriate softkey.

FLIGHT
MANAGEMENT

2) Turn the FMS Knob to place the cursor on the desired NAV identifier or NAV frequency.
3) On the Nearest VOR and Nearest Airports pages, press the FREQ Softkey to place the cursor on the NAV
frequency (Figure 4-25).
4) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio.

HAZARD
AVOIDANCE

5) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field.

AFCS

Turn the FMS
Knob to Scroll
Through a List
of Frequencies

Press the ENT
Key to Load
a Highlighted
Frequency into
the NAV Standby
Frequency Box

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 4-23 NAV Frequency Auto-Tuning from the MFD

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SYSTEM
OVERVIEW

Or:

1) When on the NRST pages, press the MENU Key to display the page menu.
2) Turn the large FMS Knob to scroll through the menu options.

FLIGHT
INSTRUMENTS

3) Press the ENT Key to place the cursor in the desired window.
4) Scroll through the frequency selections with the FMS Knob or the ENT Key.
5) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio.
6) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Nearest Airports Menu

Nearest VOR Menu

Figure 4-24 Nearest Pages Menus
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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109

SYSTEM
OVERVIEW

Audio Panel and CNS

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

In the example shown, the VOR list is selected with the VOR Softkey or from the page menu. The FMS Knob
or ENT Key is used to scroll through the list. The cursor is placed on the frequency with the FREQ Softkey and
loaded into the NAV Tuning Box with the ENT Key.

FLIGHT
MANAGEMENT

Press the ENT
Key to Load
the Frequency
into the NAV
Standby Field.

HAZARD
AVOIDANCE

Press the VOR
Softkey to Place
the Cursor on the
VOR Identifier

Press the FREQ
Softkey to Place
the Cursor on the
VOR Frequency

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-25 Loading the NAV Frequency from the NRST – Nearest VOR Page

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Audio Panel and CNS
SYSTEM
OVERVIEW

While enroute, NAV frequencies can also be auto-tuned from the NRST – Nearest Airports,
WPT – Airport Information, WPT – VOR Information, and NRST – Nearest Frequencies Pages on the MFD in
a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 4-26 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and
NRST – Nearest Airports Pages

INDEX

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SYSTEM
OVERVIEW

Audio Panel and CNS
Auto-Tuning NAV Frequencies on Approach Activation

FLIGHT
INSTRUMENTS

NOTE: The primary NAV frequency is auto-tuned upon loading a VOR or ILS/Localizer approach.
NOTE: When an ILS/LOC approach has been activated while navigating by GPS, the system automatically

switches to LOC as the final approach course is intercepted (within 15 nm of the FAF). See the Flight
Management Section for details.
NAV frequencies are automatically loaded into the NAV Frequency Box on approach activation.

EIS

When loading or activating a VOR or ILS/LOC approach, the approach frequency is automatically transferred
to a NAV frequency field as follows:

AUDIO PANEL
& CNS

• If the current CDI navigation source is GPS, the approach frequency is transferred to the NAV1 active
frequency field. The frequency that was previously in the NAV1 active frequency field is transferred to
standby.

FLIGHT
MANAGEMENT

• If the current CDI navigation source is GPS, and if the approach frequency is already loaded into the NAV1
standby frequency field, the standby frequency is transferred to active.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

• If the current CDI navigation source is NAV1 or NAV2, the approach frequency is transferred to the standby
frequency fields of the selected CDI NAV radio.

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SYSTEM
OVERVIEW

Marker Beacon Receiver
NOTE: The marker beacon indicators operate independently of marker beacon audio and cannot be turned

FLIGHT
INSTRUMENTS

off.
The marker beacon receiver is used as part of the ILS. The marker beacon receiver is always on and detects
any marker beacon signals within the reception range of the aircraft.
The receiver detects the three marker tones – outer, middle, and inner – and provides the marker beacon
annunciations located to the left of the Altimeter on the PFD.
Middle Marker
Indication

Inner Marker
Indication

EIS

Outer Marker
Indication

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 4-27 Marker Beacon Annunciations on the PFD

HAZARD
AVOIDANCE

Figure 4-28 Marker Beacon Keys
AFCS

The Audio Panel provides three different states of marker beacon operation; On, Muted, and Deselected.
Pressing the MKR/MUTE Key selects and deselects marker beacon audio. The key annunciator indicates when
marker beacon audio is selected.

ADDITIONAL
FEATURES

During marker beacon audio reception, pressing the MKR/MUTE Key mutes the audio but does not affect the
marker annunciations (Figure 4-27). The marker tone is silenced, then waits for the next marker tone. The
MKR/MUTE Key Annunciator is illuminated, indicating audio muting. The audio returns when the next marker
beacon signal is received. If the MKR/MUTE Key is pressed during signal reception (O, M, I indication) while
marker beacon audio is muted, the audio is deselected and the MKR/MUTE Key Annunciator is extinguished.

APPENDICES

Pressing the HI SENS Key switches between high and low marker beacon receiver sensitivity. The HI SENS
function (annunciator illuminated) is used to provide an earlier indication when nearing a marker during an
approach. The LO SENS function (annunciator extinguished) results in a narrower marker dwell while over a
station.

INDEX

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SYSTEM
OVERVIEW

ADF/DME Tuning

FLIGHT
INSTRUMENTS

See the Flight Instruments Section for displaying the DME and bearing information windows (ADF) and
using the ADF as the source for the bearing pointer.

EIS

Audio Panel and CNS

The UHF DME frequency is tuned by pairing with a VHF NAV frequency. DME frequency pairing is automatic
and only the VHF NAV frequency is shown.

NOTE: When another auxiliary window is turned on, the ADF/DME Tuning Window is replaced on the PFD.

The G1000 system tunes the ADF receiver (optional) and DME transceiver (optional). The ADF is tuned by
entering the frequency in the ADF standby frequency field of the ADF/DME Tuning Window. (The softkey may
be labeled ADF/DME, ADF, or DME, depending on installed equipment.)

AUDIO PANEL
& CNS

The following ADF/DME information is displayed in the ADF/DME Tuning Window:
• Active and standby ADF frequencies
• ADF receiver mode
• ADF receiver volume

FLIGHT
MANAGEMENT

• DME tuning mode (DME transceiver pairing)
When the ADF/DME Tuning Window is displayed, the selection cursor is placed over the standby ADF
frequency field.

HAZARD
AVOIDANCE

Turning the large FMS Knob moves the selection cursor through the various fields (standby ADF frequency,
ADF receiver mode, ADF radio volume, and DME tuning mode). Pressing the FMS Knob activates/deactivates
the selection cursor in the ADF/DME Tuning Window. The ADF frequency is entered using the FMS Knob and
the ENT Key.

AFCS

Active ADF Frequency

Standby ADF Frequency

ADF
Mode

ADF
Volume

ADDITIONAL
FEATURES

DME
Tuning
Mode

INDEX

APPENDICES

Figure 4-29 ADF/DME Tuning Window

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Audio Panel and CNS
SYSTEM
OVERVIEW

ADF Tuning
ADF frequencies in the 190.0-kHz to 1799.5-kHz range are entered in the standby ADF frequency field of the
ADF/DME Tuning Window. The G1000 System does not tune the ADF emergency frequency, 2182.0‑kHz.

FLIGHT
INSTRUMENTS

Tuning an ADF frequency:
1) Press the ADF/DME Softkey to display the ADF/DME Tuning Window.
2) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field.
3) Turn the small FMS Knob to begin data entry and change each digit.

EIS

4) Turn the large FMS Knob to move the cursor to the next digit position.
5) Press the ENT Key to complete data entry for the standby frequency.

Turn the Small
FMS Knob to
Enter Data in
the Standby ADF
Frequency Field

AUDIO PANEL
& CNS

Press the
ENT Key to
Complete ADF
Frequency Entry

FLIGHT
MANAGEMENT

Turn the Large
FMS Knob
to Move the
Cursor to the
Next Character

Figure 4-30 Entering ADF Standby Frequencies

HAZARD
AVOIDANCE

Pressing the CLR Key before completing frequency entry cancels the frequency change and reverts back to
the previously entered frequency.
Pressing the CLR Key when the cursor is flashing, clears the frequency and replaces the standby field with
0000.0.

AFCS

Transferring the active and standby ADF frequencies:
1) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field.
2) Press the ENT Key to complete the frequency transfer.

ADDITIONAL
FEATURES

Press the ENT
Key to Transfer
the ADF
Frequencies

APPENDICES

Figure 4-31 Transferring ADF Frequencies

INDEX

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115

SYSTEM
OVERVIEW

Selecting ADF Receiver Mode

FLIGHT
INSTRUMENTS

Audio Panel and CNS

• ANT (Antenna) – The ADF bearing pointer parks on the HSI at 90 degrees. Best mode for listening to NDB
audio.

The following modes can be selected: (In all modes NDB audio can be heard by selecting the ADF Key on
the Audio Panel.)

• ADF (Automatic Direction Finder) – The ADF pointer points to the relative bearing of the NDB station.

EIS

• ADF/BFO (ADF/Beat Frequency Oscillator) – The ADF pointer points to the relative bearing of the NDB
station and an audible tone confirms signal reception. This mode allows identification of the interrupted
carrier beacon stations used in various parts of the world.

AUDIO PANEL
& CNS

• ANT/BFO (Antenna/Beat Frequency Oscillator) – The ADF bearing pointer parks on the HSI at 90 degrees
while an audible tone is provided when a signal is received. This mode also allows identification of the
interrupted carrier beacon stations and confirms signal reception.
Selecting an ADF receiver mode:
1) Turn the large FMS Knob to place the selection cursor over the ADF mode field.

FLIGHT
MANAGEMENT

2) Turn the small FMS Knob to select the desired ADF receiver mode.

HAZARD
AVOIDANCE

Turn the Small
FMS Knob
to Select the
Mode

Figure 4-32 Selecting ADF Receiver Mode
AFCS

ADF receiver volume level can be adjusted in the tuning window from 0 to 100%. The default volume level
is set to 50%. The ADF volume level is the same for both Audio Panels.

ADDITIONAL
FEATURES

Adjusting ADF receiver volume:
1) Turn the large FMS Knob to place the selection cursor over the ADF volume field.
2) Turn the small FMS Knob to adjust volume as desired.

INDEX

APPENDICES

Turn the Small
FMS Knob
to Select the
Volume

Figure 4-33 Adjusting ADF Receiver Volume

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SYSTEM
OVERVIEW

DME Tuning
NOTE: When turning on the G1000 for use, the system remembers the last frequency used for DME tuning

FLIGHT
INSTRUMENTS

and the NAV1, NAV2, or HOLD state prior to shutdown.
The DME transceiver is tuned by selecting NAV1, NAV2, or HOLD in the ADF/DME Tuning Window.

EIS

DME
Modes

AUDIO PANEL
& CNS

Figure 4-34 ADF/DME Tuning Window, DME Modes

The following DME transceiver pairing can be selected:

FLIGHT
MANAGEMENT

• NAV1 – Pairs the DME frequency from the selected NAV1 frequency.
• NAV2 – Pairs the DME frequency from the selected NAV2 frequency.
• HOLD – When in the HOLD position, the DME frequency remains paired with the last selected NAV
frequency.

HAZARD
AVOIDANCE

Selecting DME transceiver pairing:
1) Press the ADF/DME Softkey to display the ADF/DME Tuning Window.
2) Turn the small FMS Knob to select the DME tuning mode.
3) Press the ENT Key to complete the selection.

AFCS

Pressing the CLR Key or FMS Knob while in the process of DME pairing cancels the data entry and reverts
back to the previously selected DME tuning state. Pressing the FMS Knob activates/deactivates the cursor in
the ADF/DME Tuning Window.

ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Audio Panel and CNS

4.4 GTX 33 Mode S Transponder

FLIGHT
INSTRUMENTS

The GTX 33 Mode S Transponder provides Mode A, Mode C, and Mode S interrogation and reply capabilities.
Selective addressing or Mode Select (Mode S) capability includes the following features:
• Level-2 reply data link capability (used to exchange information between aircraft and ATC facilities)
• Surveillance identifier capability
• Altitude reporting
• Airborne status determination

EIS

• Transponder capability reporting
• Mode S Enhanced Surveillance (EHS) requirements

AUDIO PANEL
& CNS

• Acquisition squitter – Acquisition squitter, or short squitter, is the transponder 24-bit identification address.
The transmission is sent periodically, regardless of the presence of interrogations. The purpose of acquisition
squitter is to enable Mode S ground stations and aircraft equipped with a Traffic Avoidance System (TAS) to
recognize the presence of Mode S-equipped aircraft for selective interrogation.

FLIGHT
MANAGEMENT

The Hazard Avoidance Section provides more details on traffic avoidance systems.

Transponder Controls

HAZARD
AVOIDANCE

Transponder function is displayed on three levels of softkeys on the PFD: Top-level, Mode Selection, and
Code Selection. When the top-level XPDR Softkey is pressed, the Mode Selection softkeys appear: STBY, ON,
ALT, VFR, CODE, IDENT, BACK.
When the CODE Softkey is pressed, the number softkeys appear: 0, 1, 2, 3, 4, 5, 6, 7, IDENT, BKSP,
BACK. The digits 8 and 9 are not used for code entry. Pressing the numbered softkeys in sequence enters the
transponder code. If an error is made, the code selection cursor can be moved back to the left one digit with
each press of the BKSP Softkey.

AFCS

Pressing the BACK Softkey during code selection reverts to the Mode Selection Softkeys. Pressing the BACK
Softkey during mode selection reverts to the top-level softkeys.

ADDITIONAL
FEATURES

The code can also be entered with the FMS Knob on the PFD. Code entry must be completed with either the
softkeys or the FMS Knob, but not a combination of both.
Pressing the IDENT Softkey while in Mode or Code Selection initiates the ident function and reverts to the
top-level softkeys.

INDEX

APPENDICES

After 45 seconds of transponder softkey inactivity, the system reverts back to the top-level softkeys.

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Audio Panel and CNS

ALT

GND

VFR

CODE

IDENT

BACK

FLIGHT
INSTRUMENTS

IDENT

SYSTEM
OVERVIEW

STBY

XPDR

ALERTS

Pressing the BACK Softkey
returns to the top-level softkeys.

IDENT

BKSP

BACK

ALERTS

EIS

Pressing the BACK Softkey returns to the mode selection softkeys.

AUDIO PANEL
& CNS

Figure 4-35 Transponder Softkeys (PFD)

Transponder Mode Selection

FLIGHT
MANAGEMENT

Mode selection can be automatic (Ground and Altitude Modes) or manual (Standby, ON, and Altitude Modes).
The STBY, ON, and ALT Softkeys can be accessed by pressing the XPDR Softkey.
Selecting a transponder mode:

HAZARD
AVOIDANCE

1) Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2) Press the desired softkey to activate the transponder mode.

Ground Mode

AFCS

Ground Mode is normally selected automatically when the aircraft is on the ground. The transponder
powers up in the last mode it was in when shut down. Ground Mode can be overridden by pressing any one
of the Mode Selection Softkeys. A green GND indication and transponder code appear in the mode field of
the Transponder Data Box. In Ground Mode, the transponder does not allow Mode A and Mode C replies,
but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations.

ADDITIONAL
FEATURES

When Standby Mode has been selected on the ground, the transponder can be returned to Ground Mode
by pressing the GND Softkey.
GND
Mode

APPENDICES

Figure 4-36 Ground Mode

INDEX

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119

SYSTEM
OVERVIEW

Standby Mode (Manual)

FLIGHT
INSTRUMENTS

Audio Panel and CNS

Standby Mode can be selected at any time by pressing the STBY Softkey. In Standby, the transponder does
not reply to interrogations, but new codes can be entered. When Standby is selected, a white STBY indication
and transponder code appear in the mode field of the Transponder Data Box. In all other modes, these fields
appear in green.

NOTE: In Standby Mode, the IDENT function is inoperative.

EIS

STBY Mode (White
Code Number and
Mode)

AUDIO PANEL
& CNS

Figure 4-37 Standby Mode

Manual ON Mode

FLIGHT
MANAGEMENT

ON Mode can be selected at any time by pressing the ON Softkey. ON Mode generates Mode A and Mode S
replies, but Mode C altitude reporting is inhibited. In ON Mode, a green ON indication and transponder
code appear in the mode field of the Transponder Data Box.

HAZARD
AVOIDANCE

ON Mode
(No Altitude
Reporting)

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-38 ON Mode

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SYSTEM
OVERVIEW

Altitude Mode (Automatic or Manual)
Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be
selected manually by pressing the ALT Softkey.

FLIGHT
INSTRUMENTS

If Altitude Mode is selected, a green ALT indication and transponder code appear in the mode field of the
Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure
altitude information.
ALT Mode
(Mode C Altitude
Reporting)

EIS

Figure 4-39 Altitude Mode
AUDIO PANEL
& CNS

Reply Status
When the transponder sends replies to interrogations, a white R indication appears momentarily in the
reply status field of the Transponder Data Box.

FLIGHT
MANAGEMENT

Reply to
Interrogation

HAZARD
AVOIDANCE

Figure 4-40 Reply Indication

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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121

SYSTEM
OVERVIEW

Audio Panel and CNS

Entering a Transponder Code
Entering a transponder code with softkeys:

FLIGHT
INSTRUMENTS

1) Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2) Press the CODE Softkey to display the Transponder Code Selection Softkeys, for digit entry.

EIS

3) Press the digit softkeys to enter the code in the code field. When entering the code, the next softkey in sequence
must be pressed within 10 seconds, or the entry is cancelled and restored to the previous code. Pressing the
BKSP Softkey moves the code selection cursor to the previous digit. Five seconds after the fourth digit has been
entered, the transponder code becomes active.

AUDIO PANEL
& CNS

Entering
a Code

Figure 4-41 Entering a Code

FLIGHT
MANAGEMENT

Entering a transponder code with the PFD FMS Knob:
1) Press the XPDR and the CODE Softkeys as in the previous procedure to enable code entry.
2) Turn the small FMS Knob on the PFD to enter the first two code digits.
3) Turn the large FMS Knob to move the cursor to the next code field.

HAZARD
AVOIDANCE

4) Enter the last two code digits with the small FMS Knob.
5) Press the ENT Key to complete code digit entry.

AFCS

Pressing the CLR Key or small FMS Knob before code entry is complete cancels code entry and restores the
previous code. Waiting for 10 seconds after code entry is finished activates the code automatically.

ADDITIONAL
FEATURES

Turn the Small
FMS Knob to
Enter Two Code
Digits at a Time

Press the
ENT Key to
Complete
Code Entry
Turn the Large
FMS Knob
to Move the
Cursor to the
Next Code Field

INDEX

APPENDICES

Figure 4-42 Entering a Code with the FMS Knob

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Audio Panel and CNS
SYSTEM
OVERVIEW

VFR Code

FLIGHT
INSTRUMENTS

The VFR code can be entered either manually or by pressing the XPDR Softkey, then the VFR Softkey.
When the VFR Softkey is pressed, the pre-programmed VFR code is automatically displayed in the code field
of the Transponder Data Box. Pressing the VFR Softkey again restores the previous identification code.
The pre-programmed VFR Code is set at the factory to 1200. If a VFR code change is required, contact a
Garmin-authorized service center for configuration.
VFR Code

EIS

Figure 4-43 VFR Code
AUDIO PANEL
& CNS

IDENT Function
NOTE: In Standby Mode, the IDENT Softkey is inoperative.

FLIGHT
MANAGEMENT

Pressing the IDENT Softkey sends a distinct identity indication to Air Traffic Control (ATC). The indication
distinguishes the identing transponder from all the others on the air traffic controller’s screen. The IDENT
Softkey appears on all levels of transponder softkeys. When the IDENT Softkey is pressed, a green IDNT
indication is displayed in the mode field of the Transponder Data Box for a duration of 18 seconds.

HAZARD
AVOIDANCE

After the IDENT Softkey is pressed while in Mode or Code Selection, the system reverts to the top-level
softkeys.
IDNT
Indication

AFCS

Press the
IDENT Softkey
to Initiate the
ID Function
Figure 4-44 IDENT Softkey and Indication

ADDITIONAL
FEATURES
APPENDICES
INDEX

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123

SYSTEM
OVERVIEW

Audio Panel and CNS

4.5 Additional Audio Panel Functions

FLIGHT
INSTRUMENTS

Power-Up
The Audio Panel performs a self-test during power-up. During the self-test all Audio Panel annunciator lights
illuminate for approximately two seconds. Once the self-test is completed, most of the settings are restored to
those in use before the unit was last turned off.

Mono/Stereo Headsets
EIS

Stereo headsets are recommended for use in this aircraft.

AUDIO PANEL
& CNS

Using a monaural headset in a stereo jack shorts the right headset channel output to ground. While this does
not damage the Audio Panel, a person listening on a monaural headset hears only the left channel in both ears.
If a monaural headset is used at one of the passenger positions, any other passenger using a stereo headset hears
audio in the left ear only.

Speaker

FLIGHT
MANAGEMENT

All of the radios can be heard over the cabin speaker. Pressing the SPKR Key selects and deselects the cabin
speaker. Speaker audio is muted when the PTT is pressed. Certain aural alerts and warnings (autopilot, traffic,
altitude) are always heard on the speaker, even when the speaker is not selected.

HAZARD
AVOIDANCE

The speaker volume is adjustable within a nominal range. Contact a Garmin-authorized service center for
volume adjustment.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-45 Passenger Address and Speaker Keys

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Audio Panel and CNS
SYSTEM
OVERVIEW

Intercom

FLIGHT
INSTRUMENTS

The Audio Panel includes a four-position intercom system (ICS) and a stereo music input for the pilot, copilot
and up to two passengers. The intercom provides Pilot and Copilot isolation from the passengers and aircraft
radios.

OFF

Pilot Hears

Passenger Hears

Selected radios, aural
alerts, pilot, copilot,
passengers, music

Selected radios, aural alerts,
pilot, copilot, passengers,
music

OFF

Selected radios, aural
alerts, pilot

Copilot, passengers,
music

OFF

Selected radios, aural
alerts, pilot; passengers, Copilot
music

Selected radios, aural alerts,
pilot, passengers,
music

Selected radios, aural
alerts, pilot, copilot

Passengers;
music

Selected radios, aural
alerts, pilot, copilot

HAZARD
AVOIDANCE

Copilot Hears

FLIGHT
MANAGEMENT

COPLT KEY
Annunciator

AUDIO PANEL
& CNS

PILOT KEY
Annunciator

EIS

Figure 4-46 Intercom Controls

AFCS

Table 4-1 ICS Isolation Modes

ADDITIONAL
FEATURES

Pilot isolation is selected when the PILOT Annunciator is illuminated. During Pilot isolation, the pilot can
hear the selected radios and aural alerts and warnings. The copilot and passengers can communicate with each
other. The copilot is isolated from aural alerts and warnings.
Copilot isolation is selected when the COPLT Annunciator is illuminated. The copilot is isolated from the
selected radios, aural alerts and warnings, and everyone else. The pilot and passengers can hear the selected
radios and communicate with each other.

APPENDICES

When both the PILOT and COPLT Annunciators are illuminated, the pilot and copilot can hear the selected
radios and communicate with each other. The passengers are isolated from the pilot and copilot but can
communicate with each other.

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

When both the PILOT and COPLT Annunciators are extinguished, everyone hears the selected radios and is
able to communicate with everyone else.

125

SYSTEM
OVERVIEW

Audio Panel and CNS
Intercom Volume and Squelch

FLIGHT
INSTRUMENTS

The PILOT/PASS Knob controls volume or manual squelch adjustment for the pilot and copilot/passenger.
The small knob controls the pilot volume and squelch. The large knob controls the copilot/passenger volume
and squelch. The VOL and SQ annunciations at the bottom of the unit indicate which function the knob is
controlling. Pressing the PILOT/PASS Knob switches between volume and squelch control as indicated by
the VOL or SQ annunciation being illuminated.

EIS

The MAN SQ Key allows either automatic or manual control of the squelch setting. When the MAN SQ
Annunciator is extinguished (Automatic Squelch is on), the PILOT/PASS Knob controls only the volume
(pressing the PILOT/PASS Knob has no effect on the VOL/SQ selection).
When the MAN SQ Annunciator is illuminated (Manual Squelch), the PILOT/PASS Knob controls both
volume and squelch.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Manual Squelch Annunciator;
Off for Automatic Squelch, On
for Manual Squelch
Automatic/Manual Squelch

HAZARD
AVOIDANCE

Pilot Volume or Manual
Squelch. Press to switch
between VOL and SQ. Turn
to adjust Squelch when SQ
Annunciation is lit, Volume
when VOL Annunciation is lit.

Copilot/Passenger
Volume or
Manual Squelch

Volume Annunciation

Squelch Annunciation

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 4-47 Volume/Squelch Control

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Audio Panel and CNS
SYSTEM
OVERVIEW

Passenger Address (PA) System

FLIGHT
INSTRUMENTS

A passenger address system is available for delivering voice messages over the cabin speaker. When the PA
Key is selected on the Audio Panel, the COM MIC Annunciator is extinguished, and the active COM frequency
changes to white, indicating that there is no COM selected. A Push-to-Talk (PTT) must be pressed to deliver PA
announcements. The PA Annunciator flashes about once per second while the PTT is depressed.

EIS

PA Key is Selected on
the Audio Panel

AUDIO PANEL
& CNS

Figure 4-49 PA Key Selected for Cabin Announcements

FLIGHT
MANAGEMENT

Clearance Recorder and Player
The Audio Panel contains a digital clearance recorder that continually records up to 2.5 minutes of the
selected COM radio signal. Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of
recording time have been reached, the recorder begins recording over the stored memory blocks, starting from
the oldest block.

HAZARD
AVOIDANCE

The PLAY Key controls the play function. Pressing the PLAY Key once plays the latest recorded memory
block. The PLAY Annunciator flashes to indicate when play is in progress. The PLAY Annunciator turns off
after the present memory block has finished playing.
Pressing the MKR/MUTE Key during play of a memory block stops play. If a COM input signal is detected
during play of a recorded memory block, play is halted.

AFCS

Pressing the PLAY Key while audio is playing begins playing the previously recorded memory block. Each
subsequent press of the PLAY Key selects the previously recorded memory block.
Powering off the unit automatically clears all recorded blocks.

ADDITIONAL
FEATURES

MKR/MUTE
Key Stops Play

APPENDICES

PLAY Key
Controls the
Play Function

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Figure 4-49 Marker Mute and Play Keys

127

SYSTEM
OVERVIEW

Audio Panel and CNS

Entertainment Inputs
NOTE: The entertainment MUSIC INPUT cannot be completely turned off. Audio level for MUSIC INPUT can

FLIGHT
INSTRUMENTS

be adjusted by a Garmin-authorized service center.
The Audio Panel provides a stereo entertainment input from the data link receiver or an MUSIC INPUT jack
for the crew and passengers. The MUSIC INPUT jack input is compatible with popular portable entertainment
devices such as MP3 and CD players through a 3.5-mm stereo phone jack, installed in a convenient location.
The headphone outputs of the entertainment devices are plugged into the MUSIC INPUT jack.

EIS

The current ICS state of isolation affects the distribution of the entertainment input (see Table 4‑1).

Crew Music
AUDIO PANEL
& CNS

Music can be heard by the pilot and copilot when both the PILOT and the COPLT ICS Annunciators are
extinguished. Music can also be heard by the pilot when the COPLT Annunciator is illuminated and by the
copilot when the PILOT Annunciator is illuminated.

FLIGHT
MANAGEMENT

Music Muting
Music muting occurs when aircraft radio or marker beacon activity is heard. Music is always soft muted
when an interruption occurs from these sources. Soft muting is the gradual return of music to its original
volume level. The time required for music volume to return to normal is between one-half and four
seconds.

HAZARD
AVOIDANCE

Music Muting Enable/Disable
Pressing and holding the MKR/MUTE Key for three seconds switches music muting on and off. When
switching, either one or two beeps are heard; one beep indicates that music muting is enabled, two beeps
indicate music muting is disabled. Music muting is reset (enabled) during power up.

AFCS

Passenger Music
Music can be heard only by the passengers and is never muted.

ADDITIONAL
FEATURES

XM Radio Entertainment
XM Radio audio from the Data Link Receiver may be heard by the pilot and passengers simultaneously
(optional: requires subscription to XM Radio Service). Refer to the Additional Features Section for more
details on the Data Link Receiver.

INDEX

APPENDICES

Connecting a stereo input to the MUSIC INPUT jack removes the XM Radio Audio from that input.

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SYSTEM
OVERVIEW

4.6 Audio Panel Preflight Procedure

FLIGHT
INSTRUMENTS

NOTE: If the pilot and/or copilot are using headsets that have a high/low switch or volume control knob,

verify that the switch is in the high position and the volume control on the headsets are at maximum volume
setting. On single‑pilot flights, verify that all other headsets are not connected to avoid excess noise in the
audio system.
NOTE: When the MAN SQ Key is pressed, the ICS squelch can be set manually by the pilot and copilot. If

EIS

manual squelch is set to full open (SQ annunciated and the knobs turned counterclockwise) background
noise is heard in the ICS system as well as during COM transmissions.

AUDIO PANEL
& CNS

After powering up the G1000 System, the following steps aid in maximizing the use of the Audio Panel as well
as prevent pilot and copilot induced issues. These preflight procedures should be performed each time a pilot
boards the aircraft to insure awareness of all audio levels in the Audio Panel and radios.

FLIGHT
MANAGEMENT

Automatic/Manual
Squelch
Pilot and
Copilot ICS
Isolation Keys

HAZARD
AVOIDANCE

Pilot Volume
or Manual
Squelch

Copilot/Passenger
Volume or
Manual Squelch

AFCS

Squelch
Annunciation

Volume
Annunciation
Figure 4-50 Audio Panel Controls

ADDITIONAL
FEATURES

Setting the Audio Panel during preflight:
1) Verify that the PILOT and COPLT Annunciators are extinguished.
2) Verify that the MAN SQ Annunciator is extinguished.

APPENDICES

3) Turn the PILOT/PASS Knobs clockwise two full turns. This sets the headset intercom audio level to max volume
(least amount of attenuation).
4) Adjust radio volume levels (COM, NAV, etc.) to a suitable level.
5) Adjust the PILOT/PASS Knob volume to the desired intercom level.

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INDEX

Once this procedure has been completed, the pilot and copilot can change settings, keeping in mind the notes
above.

129

SYSTEM
OVERVIEW

Audio Panel and CNS

4.7 Abnormal Operation

FLIGHT
INSTRUMENTS

Abnormal operation of the G1000 includes equipment failures of the G1000 components and failure of
associated equipment, including switches and external devices.

Stuck Microphone
If the push-to-talk (PTT) Key becomes stuck, the COM transmitter stops transmitting after 35 seconds of
continuous operation. An alert appears on the PFD to advise the pilot of a stuck microphone.

AUDIO PANEL
& CNS

EIS

The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel flashes as long as the PTT Key remains
stuck.

FLIGHT
MANAGEMENT

Figure 4-51 Stuck Microphone Alert

COM Tuning Failure

HAZARD
AVOIDANCE

In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is automatically tuned in
the radio in which the tuning failure occurred. Depending on the failure mode, a red X may appear on the
frequency display.
Emergency Channel
Loaded Automatically

AFCS

Figure 4-52 COM Tuning Failure

Audio Panel Fail-Safe Operation

ADDITIONAL
FEATURES

If there is a failure of the Audio Panel, a fail-safe circuit connects the pilot’s headset and microphone directly
to the COM1 transceiver. Audio is not available on the speaker during Fail-safe operation.

Reversionary Mode

INDEX

APPENDICES

The red DISPLAY BACKUP Button selects the Reversionary Mode. See the System Overview Section for
more information on Reversionary Mode.

Figure 4-53 Display Backup Button

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Flight Management
SYSTEM
OVERVIEW

Section 5 Flight Management

FLIGHT
INSTRUMENTS

5.1 Introduction
The G1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of
the Pilot’s Guide explains flight management using the G1000.

EIS

The most prominent part of the G1000 are the two full color displays: a Primary Flight Display (PFD) and a
Multi Function Display (MFD). The information to successfully navigate the aircraft using the GPS sensors is
displayed on the PFD and the MFD. See examples in the Figure 5-1 and Figure 5-2. Detailed descriptions of flight
management functions are discussed later in this section.
A brief description of the flight management data on the PFD and MFD follows.

AUDIO PANEL
& CNS

Navigation mode indicates which sensor is providing the course data (e.g., GPS, VOR) and the flight plan phase
(e.g., Departure (DPRT), Terminal (TERM), Enroute (ENR), Oceanic (OCN), Approach (LNAV, LNAV+V, L/VNAV,
or LPV), or Missed Approach (MAPR)).

FLIGHT
MANAGEMENT

The Inset Map is a small version of the MFD Navigation Map and can be displayed in the lower left corner of
the PFD. When the system is in reversionary mode, the Inset Map is displayed in the lower right corner. The
Inset Map is displayed by pressing the INSET Softkey. Selecting the INSET Softkey again, then selecting the OFF
Softkey removes the Inset Map.

HAZARD
AVOIDANCE

The Navigation Map displays aviation data (e.g., airports, VORs, airways, airspaces), geographic data (e.g.,
cities, lakes, highways, borders), topographic data (map shading indicating elevation), and hazard data (e.g.,
traffic, terrain, weather). The amount of displayed data can be reduced by selecting the DCLTR Softkey. The
Navigation Map can be oriented four different ways: North Up (NORTH UP), Track Up (TRK UP), Desired Track
Up (DTK UP), or Heading Up (HDG UP).

AFCS

An aircraft icon is placed on the Navigation Map at the location corresponding to the calculated present position.
The aircraft position and the flight plan legs are accurately based on GPS calculations. The basemap upon which
these are placed are from a source with less resolution, therefore the relative position of the aircraft to map features
is not exact. The leg of the active flight plan currently being flown is shown as a magenta line on the navigation
map. The other legs are shown in white.

ADDITIONAL
FEATURES

There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in the
lower right corner of the map and represents the top-to-bottom distance covered by the map. To change the map
range on any map, turn the Joystick counter-clockwise to zoom in ( -, decreasing), or clockwise to zoom out (+,
increasing).

APPENDICES

The Direct-to Window, the Flight Plan Window, the Procedures Window, and the Nearest Airports Window
can be displayed in the lower right corner of the PFD. Details of these windows are discussed in detail later in
the section.

INDEX

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OVERVIEW

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FLIGHT
INSTRUMENTS

Navigation Status Box

Navigation Mode
Inset Map

AUDIO PANEL
& CNS

EIS

Location of:
- Direct To Window
- Flight Plan Window
- Procedures Window
- Nearest Airports Window
Figure 5-1 GPS Navigation Information on the PFD

FLIGHT
MANAGEMENT

Navigation Status Box
Map Orientation

Navigation Page Title
Navigation Map

HAZARD
AVOIDANCE

- Aviation Data
- Geographic Data
- Topographic Data
- Hazard Data

Flight Plan Leg
Aircraft Icon
at Present Position

ADDITIONAL
FEATURES

AFCS

Active Flight Plan Leg

Map Range

INDEX

APPENDICES

Figure 5-2 GPS Navigation Information on the MFD Navigation Page

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SYSTEM
OVERVIEW

Navigation Status Box
The Navigation Status Box located at the top of the PFD contains two fields displaying the following
information:

FLIGHT
INSTRUMENTS

PFD Navigation Status Box

The Navigation Status Box located at the top of the
MFD contains four data fields, each displaying one of
the following items:

• Distance (DIS) and Bearing (BRG) to the next
waypoint or flight plan annunciations (e.g., ‘TOD
within 1 minute’)

• Bearing (BRG)

Symbol

Description
Active Leg

• Distance (DIS)
• Desired Track (DTK)

AUDIO PANEL
& CNS

The symbols used in the PFD status bar are:

EIS

• Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD > KCOS’) or flight plan annunciations (e.g., ‘Turn
right to 021˚ in 8 seconds’)

• Enroute Safe Altitude (ESA)
• Estimated Time of Arrival (ETA)

Direct-to

FLIGHT
MANAGEMENT

• Estimated Time Enroute (ETE)
• Ground Speed (GS)

Right Procedure Turn
Left Procedure Turn

• True Air Speed (TAS)
• Track Angle Error (TKE)

HAZARD
AVOIDANCE

Right Holding Pattern

• Minimum Safe Altitude (MSA)

• Track (TRK)

Left Holding Pattern

• Vertical Speed Required (VSR)

Vector to Final

• Crosstrack Error (XTK)
AFCS

Right DME Arc
Left DME Arc

ADDITIONAL
FEATURES

MFD Navigation Status Box

APPENDICES

The navigation information displayed in the four data fields can be selected on the MFD Data Bar Fields Box
on the AUX - System Setup Page. The default selections (in order left to right) are GS, DTK, TRK, and ETE.
Changing a field in the MFD Navigation Status Box:
1) Select the System Setup Page.

INDEX

2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box.

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4) Turn the small FMS Knob to display and scroll through the data options list.
5) Select the desired data.

FLIGHT
INSTRUMENTS

6) Press the ENT Key. Pressing the DFLTS Softkey returns any field to its default setting.

5.2 Using Map Displays

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Map displays are used extensively in the G1000 to provide situational awareness in flight. Most G1000 maps
can display the following information:
• Airports, NAVAIDs, airspaces, airways, land data • Icons for enabled map features
(highways, cities, lakes, rivers, borders, etc.) with • Aircraft icon (representing present position)
names
• Nav range ring
• Map Pointer information (distance and bearing to
pointer, location of pointer, name, and other pertinent • Flight plan legs
information)
• User waypoints
• Map range
• Track vector
• Wind direction and speed

• Topography scale

• Map orientation

• Topography data

HAZARD
AVOIDANCE

The information in this section applies to the following maps unless otherwise noted:
• All Map Group Pages (MAP)

• Flight Plan Pages (FPL)

• All Waypoint Group Pages (WPT)

• Direct-to Window

• AUX - Trip Planning

• PFD Inset Map

• All Nearest Group Pages (NRST)

• Procedure Loading Pages

AFCS

Map Orientation

INDEX

APPENDICES

ADDITIONAL
FEATURES

Maps are shown in one of four different orientation options, allowing flexibility in determining aircraft
position relative to other items on the map (north up) or for determining where map items are relative to where
the aircraft is going (track up, desired track up, or heading up). The map orientation is shown in the upper
right corner of the map.

Figure 5-3 Map Orientation

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Flight Management
SYSTEM
OVERVIEW

• North up (NORTH UP) aligns the top of the map display to north (default setting).
• Track up (TRK UP) aligns the top of the map display to the current ground track.
• Desired track up (DTK UP) aligns the top of the map display to the desired course.

FLIGHT
INSTRUMENTS

• Heading up (HDG UP) aligns the top of the map display to the current aircraft heading.
Note: When panning or reviewing active flight plan legs in a non-North Up orientation, the map does not

show the map orientation nor the wind direction and speed.

EIS

Note: Map orientation can only be changed on the Navigation Map Page. Any other displays that show

navigation data reflect the orientation selected for the Navigation Map Page:

AUDIO PANEL
& CNS

Changing the Navigation Map orientation:
1) With the Navigation Map Page displayed, press the MENU Key. The cursor flashes on the ‘Map Setup’ option.

FLIGHT
MANAGEMENT

Map Setup
Selection

HAZARD
AVOIDANCE

Figure 5-4 Navigation Map Page Menu Window

2) Press the ENT Key to display the Map Setup Window.
3) Turn the large FMS Knob, or press the ENT Key once, to select the ‘ORIENTATION’ field.

AFCS

Map Group Selection
Orientation Field

ADDITIONAL
FEATURES
APPENDICES

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INDEX

Figure 5-5 Map Setup Menu Window - Map Group

135

SYSTEM
OVERVIEW

Flight Management
4) Turn the small FMS Knob to select the desired orientation.
5) Press the ENT Key to select the new orientation.

FLIGHT
INSTRUMENTS

6) Press the FMS Knob to return to the base page.

Map Range

AUDIO PANEL
& CNS

EIS

There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in
the lower right corner of the map and represents the top-to-bottom distance covered by the map. When the
map range is decreased to a point that exceeds the capability of the G1000 to accurately represent the map,
a magnifying glass icon is shown to the left of the map range. To change the map range turn the Joystick
counter-clockwise to decrease the range, or clockwise to increase the range.

FLIGHT
MANAGEMENT

Range Overzoom

HAZARD
AVOIDANCE

Figure 5-6 Map Range

Auto Zoom

AFCS

Auto zoom allows the G1000 to change the map display range to the smallest range clearly showing the
active waypoint. Auto zoom can be overridden by adjusting the range with the Joystick, and remains until
the active waypoint changes, a terrain or traffic alert occurs, the aircraft takes off, or the manual override times
out (timer set on Map Setup Window).

ADDITIONAL
FEATURES

If a terrain caution or warning occurs, any map page displaying TAWS/TERRAIN data automatically adjusts
to the smallest map range clearly showing the highest priority alert. If a new traffic advisory alert occurs, any
map page capable of displaying traffic advisory alerts automatically adjusts to the smallest map range clearly
showing the traffic advisory. When terrain or traffic alerts clear, the map returns to the previous auto zoom
range based on the active waypoint.

APPENDICES

The auto zoom function can be turned on or off independently for the PFDs and MFD. Control of the
ranges at which the auto zoom occurs is done by setting the minimum and maximum ‘look forward’ times
(set on the Map Setup Window for the Map Group). These settings determines the minimum and maximum
distance to display based upon the aircraft’s ground speed.

INDEX

• Waypoints that are long distances apart cause the map range to increase to a point where many details on
the map are decluttered. If this is not acceptable, lower the maximum look ahead time to a value that limits
the auto zoom to an acceptable range.
• Waypoints that are very short distances apart cause the map range to decrease to a point where situational
awareness may not be what is desired. Increase the minimum look ahead time to a value that limits the auto
zoom to a minimum range that provides acceptable situational awareness.

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SYSTEM
OVERVIEW

• Flight plans that have a combination of long and short legs cause the range to increase and decrease as
waypoints sequence. To avoid this, auto zoom can be disabled or the maximum/minimum times can be
adjusted.

FLIGHT
INSTRUMENTS

• The ‘time out’ time (configurable on the Map Setup Page for the Map Group) determines how long auto
zoom is overridden by a manual adjustment of the range knob. At this expiration of this time, the auto
zoom range is restored. Setting the ‘time out’ value to zero causes the manual override to never time out.
• When the maximum ‘look forward’ time is set to zero, the upper limit becomes the maximum range available
(2000 nm).
• When the minimum ‘look forward’ time is set to zero, the lower limit becomes 1.5 nm.

EIS

Manual Range Override
Expiration Time

AUDIO PANEL
& CNS

Auto Zoom:

Off, MFD Only, PFD Only, All On

Maximum Look Forward Time
Minimum Look Forward Time

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom

Configuring automatic zoom:
AFCS

1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.

ADDITIONAL
FEATURES

4) Press the ENT Key.
5) Highlight the ‘AUTO ZOOM’ field.
6) Select ‘Off’, ‘MFD Only’, ‘PFD Only’, or ‘ALL On’.

APPENDICES

7) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘MAX LOOK FWD’ field.
Times are from zero to 999 minutes.
8) Use the FMS Knobs to set the time. Press the ENT Key.
9) Repeat step 8 for ‘MIN LOOK FWD’ (zero to 99 minutes) and ‘MAX LOOK FWD’ (zero to 999 minutes).
10) Press the FMS Knob to return to the Navigation Map Page.

INDEX

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Map Panning
Map panning allows the pilot to:

FLIGHT
INSTRUMENTS

• View parts of the map outside the displayed range without adjusting the map range
• Highlight and select locations on the map
• Review information for a selected airport, NAVAID or user waypoint
• Designate locations for use in flight planning
• View airspace and airway information

AUDIO PANEL
& CNS

EIS

When the panning function is selected by pressing the Joystick, the Map Pointer flashes on the map display.
A window also appears at the top of the map display showing the latitude/longitude position of the pointer,
the bearing and distance to the pointer from the aircraft’s present position, and the elevation of the land at the
position of the pointer.

FLIGHT
MANAGEMENT

Map Pointer Information

AFCS

HAZARD
AVOIDANCE

Map Pointer

ADDITIONAL
FEATURES

Figure 5-8 Navigation Map - Map Pointer Activated

Note: The map is normally centered on the aircraft’s position. If the map has been panned and there has

INDEX

APPENDICES

been no pointer movement for about 60 seconds, the map reverts back to centered on the aircraft position
and the flashing pointer is removed.

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Flight Management
SYSTEM
OVERVIEW

When the Map Pointer is placed on an object, the name of the object is highlighted (even if the name was
not originally displayed on the map). When any map feature or object is selected on the map display, pertinent
information is displayed.

FLIGHT
INSTRUMENTS

Information about Point
of Interest

EIS
AUDIO PANEL
& CNS

Map Pointer on
POI

FLIGHT
MANAGEMENT

Figure 5-9 Navigation Map - Map Pointer on Point of Interest

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

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FLIGHT
INSTRUMENTS

When the Map Pointer crosses an airspace boundary, the boundary is highlighted and airspace information
is shown at the top of the display. The information includes the name and class of airspace, the ceiling in feet
above Mean Sea Level (MSL), and the floor in feet MSL.

EIS

Information about
Airspace

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Map Pointer on
Airspace

HAZARD
AVOIDANCE

Figure 5-10 Navigation Map - Map Pointer on Airspace

Panning the map:
1) Press the Joystick to display the Map Pointer.
2) Move the Joystick to move the Map Pointer around the map.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position.

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SYSTEM
OVERVIEW

Reviewing information for an airport, NAVAID, or user waypoint:
1) Place the Map Pointer on a waypoint.
2) Press the ENT Key to display the Waypoint Information Page for the selected waypoint.

FLIGHT
INSTRUMENTS

3) Press the GO BACK Softkey, the CLR Key, or the ENT Key to exit the Waypoint Information Page and return to
the Navigation Map showing the selected waypoint.

EIS

NAVAID
Information

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

GO BACK Softkey
Figure 5-11 Navigation Map - Information Window - NAVAID

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

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Viewing airspace information for a special-use or controlled airspace:
1) Place the Map Pointer on an open area within the boundaries of an airspace.

FLIGHT
INSTRUMENTS

2) Press the ENT Key to display an options menu.
3) ‘Review Airspace?’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace
Information Page for the selected airspace.

EIS

4) Press the CLR or ENT Key to exit the Airspace Information Page.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Airspace
Information

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 5-12 Navigation Map - Information Window - Airspace

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Flight Management
SYSTEM
OVERVIEW

Measuring Bearing and Distance

FLIGHT
INSTRUMENTS

Distance and bearing from the aircraft’s present position to any point on the viewable navigation map may be
calculated using the ‘Measure Bearing and Distance’ selection from Navigation Map page menu. The bearing
and distance tool displays a dashed Measurement Line and a Measure Pointer to aid in graphically identifying
points with which to measure. Lat/Long, distance and elevation data for the Measure Pointer is provided in a
window at the top of the navigation map.
Measuring bearing and distance between any two points:
1) Press the MENU Key (with the Navigation Map Page displayed).

EIS

2) Highlight the ‘Measure Bearing/Distance’ field.
3) Press the ENT Key. A Measure Pointer is displayed on the map at the aircraft’s present position.

AUDIO PANEL
& CNS

4) Move the Joystick to place the reference pointer at the desired location. The bearing and distance are displayed
at the top of the map. Elevation at the current pointer position is also displayed. Pressing the ENT Key changes
the starting point for measuring.

Measurement
Information

FLIGHT
MANAGEMENT

5) To exit the Measure Bearing/Distance option, press the Joystick; or select ‘Stop Measuring’ from the Page
Menu and press the ENT Key.

Pointer Lat/Long

HAZARD
AVOIDANCE

Measurement Line

AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-13 Navigation Map - Measuring Bearing and Distance

INDEX

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OVERVIEW

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Topography

FLIGHT
INSTRUMENTS

All navigation maps can display various shades of topography colors representing land elevation, similar
to aviation sectional charts. Topographic data can be displayed or removed as described in the following
procedures.
Navigation Map
Topographic Data

AUDIO PANEL
& CNS

EIS

Navigation Map
Black Background

TOPO Softkey
Not Enabled
TOPO Softkey
Enabled

FLIGHT
MANAGEMENT

TOPO Off

TOPO On

Figure 5-14 Navigation Map - Topographic Data

Displaying/removing topographic data on all pages displaying navigation maps:

HAZARD
AVOIDANCE

1) Press the MAP Softkey (the INSET Softkey for the PFD Inset Map).
2) Press the TOPO Softkey.
3) Press the TOPO Softkey again to remove topographic data from the Navigation Map. When topographic data
is removed from the page, all navigation data is presented on a black background.

AFCS

Displaying/removing topographic data (TOPO DATA) using the Navigation Map Page Menu:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.

ADDITIONAL
FEATURES

3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘TOPO DATA’ field.

APPENDICES

6) Select ‘On’ or ‘Off’.

INDEX

7) Press the FMS Knob to return to the Navigation Map Page.

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Flight Management
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

TOPO DATA
Range

EIS

TOPO DATA
On/Off

AUDIO PANEL
& CNS

Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup

The topographic data range is the maximum map range on which topographic data is displayed.

FLIGHT
MANAGEMENT

Note: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the

PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g., a setting
of 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map
removes the same item at 50 nm).

HAZARD
AVOIDANCE

Selecting a topographical data range (TOPO DATA):
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.

AFCS

4) Press the ENT Key.
5) Highlight the ‘TOPO DATA’ range field. TOPO ranges are from 500 ft to 2000 nm.
6) To change the TOPO range setting, turn the small FMS Knob to display the range list.

ADDITIONAL
FEATURES

7) Select the desired range using the small FMS Knob.
8) Press the ENT Key.
9) Press the FMS Knob to return to the Navigation Map Page.

APPENDICES

In addition, the Navigation Map can display a topographic scale (located in the lower right hand side of the
map) showing a scale of the terrain elevation and current elevation values as shown following.

INDEX

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Flight Management

Maximum Displayed Elevation

FLIGHT
INSTRUMENTS

Minimum Displayed Elevation

Aircraft Altitude (MSL)
Range of
Displayed
Elevations

AUDIO PANEL
& CNS

EIS

Ground Elevation at Map Pointer
Location (only visible when Map
Pointer is displayed)

Figure 5-16 Navigation Map - TOPO SCALE

FLIGHT
MANAGEMENT

Displaying/removing the topographic scale (TOPO SCALE):
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group and press the ENT Key.

HAZARD
AVOIDANCE

4) Highlight the ‘TOPO SCALE’ field.
5) Select ‘On’ or ‘Off’.

ADDITIONAL
FEATURES

AFCS

6) Press the FMS Knob to return to the Navigation Map Page.

APPENDICES

TOPO SCALE
On/Off

INDEX

Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup

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SYSTEM
OVERVIEW

Map Symbols

FLIGHT
INSTRUMENTS

This section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol
can be turned on or off, and the maximum range to display each symbol can be set. The decluttering of the
symbols from the map using the DCLTR Softkey is also discussed.

Land Symbols
The following items are configured on the land menu:
Land Symbols

Symbol

Default
Maximum
Range (nm) Range (nm)
EIS

(Text label size can be None, Small, Medium (Med), or Large
(Lrg)

Latitude/Longitude (LAT/LON)

Off

2000

International Highway (FREEWAY)

300

800

US Highway (NATIONAL HWY)

State Highway (LOCAL HWY)

Local Road (LOCAL ROAD)

Railroads (RAILROAD)

LARGE CITY (> 200,000)

800

1500

MEDIUM CITY (> 50,000)

100

200

SMALL CITY (> 5,000)
States and Provinces (STATE/PROV)

20
800

50
1500

Rivers and Lakes (RIVER/LAKE)

200

500

USER WAYPOINT

150

300

N/A

ADDITIONAL
FEATURES

800

AFCS

300

HAZARD
AVOIDANCE

Interstate Highway (FREEWAY)

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Highways and Roads

APPENDICES

Table 5-1 Land Symbol Information

INDEX

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Aviation Symbols
The following items are configured on the aviation menu:
Aviation Symbols
FLIGHT
INSTRUMENTS

(Text label size can be None, Small, Medium (Med),
or Large (Lrg)

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Default
Maximum
Range (nm) Range (nm)

Active Flight Plan Leg (ACTIVE FPL)

2000

Non-active Flight Plan Leg (ACTIVE FPL)

2000

2000
250
150
50
3
Off
15

2000
500
300
100
20
100
30

Non-directional Beacon (NDB WAYPOINT)

VOR (VOR WAYPOINT)

150

300

Class B Airspace/TMA (CLASS B/TMA)

200

500

Class C Airspace/TCA (CLASS C/TCA)

200

500

Class D Airspace (CLASS D)

150

300

Restricted Area (RESTRICTED)

200

500

Military Operations Area [MOA(MILITARY)]

200

500

Other/Air Defense Interdiction Zone (OTHER/ADIZ)

200

500

Temporary Flight Restriction (TFR)

500

2000

Active Flight Plan Waypoint (ACTIVE FPL WPT)
Large Airports (LARGE APT)
Medium Airports (MEDIUM APT)
Small Airports (SMALL APT)
Taxiways (SAFETAXI)
Runway Extension (RWY EXTENSION)
Intersection (INT WAYPOINT)

APPENDICES

Symbol

See Airports, NAVAIDs

See Additional Features
N/A

INDEX

Table 5-2 Aviation Symbol Information

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Flight Management
SYSTEM
OVERVIEW

Symbol Setup
All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed
totally (turned off).

FLIGHT
INSTRUMENTS

Displaying/removing all land symbols:
1) Press the MENU Key with the Navigation Map Page displayed. The Page Menu is displayed and the cursor
flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Group Menu is displayed and the cursor flashes on the ‘Map’ option.

EIS

3) Highlight the ‘LAND DATA’ field.
4) Select ‘On’ or ‘Off’.
5) Press the FMS Knob to return to the Navigation Map Page.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

LAND DATA
On/Off

HAZARD
AVOIDANCE

Figure 5-18 Navigation Map Setup Menu - TOPO SCALE Setup
AFCS

The label size (TEXT) sets the size at which labels appear on the display (none, small, medium, and large).
The range (RNG) sets the maximum range at which items appear on the display.

ADDITIONAL
FEATURES

Selecting a ‘Land’ or ‘Aviation’ group item text size and range:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.

APPENDICES

3) Select the ‘Land’ or ‘Aviation’ group.
4) Press the ENT Key. The cursor flashes on the first field.
5) Select the desired land option.
6) Select the desired text size.
7) Press the ENT Key to accept the selected size.

INDEX

6) Select the desired range.

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Flight Management
7) Press the ENT Key to accept the selected range.

FLIGHT
INSTRUMENTS

8) Press the FMS Knob to return to the Navigation Map Page.

AUDIO PANEL
& CNS

EIS

Text Label Size
(None, Small Med, or Lrg)

Maximum Display Range

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup

Maximum Display Range

ADDITIONAL
FEATURES

AFCS

Text Label Size
(None, Small Med, or Lrg)

APPENDICES

Figure 5-20 Navigation Map Setup Menu - AVIATION GROUP Setup

Note: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the

INDEX

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SYSTEM
OVERVIEW

Map Declutter
The declutter feature allows the pilot to progressively step through four levels of removing map information.
The declutter level is displayed in the DCLTR Softkey and next to the Declutter Menu Option.

FLIGHT
INSTRUMENTS

Declutter Level

EIS

DCLTR Softkey
Navigation Map Page Menu
Figure 5-21 Navigation Map - Declutter Level Indications

AUDIO PANEL
& CNS

Decluttering the map:
Press the DCLTR Softkey with the Navigation Map Page displayed. The current declutter level is shown. With
each softkey selection, another level of map information is removed.

Or:

FLIGHT
MANAGEMENT

1) Press the MENU Key with the Navigation Map Page displayed.
2) Select ‘Declutter’. The current declutter level is shown.
3) Press the ENT Key.

HAZARD
AVOIDANCE

Decluttering the PFD Inset Map:
1) Press the INSET Softkey.
2) Press the DCLTR Softkey. The current declutter level is shown. With each selection, another level of map
information is removed.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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Flight Management
Table 5-3 lists the items displayed at each declutter level. The ‘X’ represents map items displayed for the
various levels of declutter.
Item

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Flight Plan Route Lines
Flight Plan Route Waypoints
Rivers/Lakes
Topography Data
International Borders
Track Vector
Navigation Range Ring
Fuel Range Ring
Terrain Data
Traffic
Airways
NEXRAD
XM Lightning Data
Airports
Runway Labels
Restricted
MOA (Military)
User Waypoints
Latitude/Longitude Grid
NAVAIDs
Class B Airspaces/TMA
Class C Airspaces/TCA
Class D Airspaces
Other Airspaces/ADIZ
TFRs
Obstacles
Land/Country Text
Cities
Roads
Railroads
State/Province Boundaries
River/Lake Names

No Declutter Declutter-1 Declutter-2 Declutter-3
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X

INDEX

Table 5-3 Navigation Map Items Displayed by Declutter Level

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Flight Management
SYSTEM
OVERVIEW

Airways

FLIGHT
INSTRUMENTS

This airways discussion is based upon the North American airway structure. The airway structure in places
other than North America vary by location, etc. and are not discussed in this book. Low Altitude Airways (or
Victor Airways) primarily serve smaller piston-engine, propeller-driven airplanes on shorter routes and at lower
altitudes. Airways are eight nautical miles wide and start 1,200 feet above ground level (AGL) and extend up
to 18,000 feet mean sea level (MSL). Low Altitude Airways are designated with a “V” before the airway number
(hence the name “Victor Airways”) since they run primarily between VORs.

EIS

High Altitude Airways (or Jet Routes) primarily serve airliners, jets, turboprops, and turbocharged piston
aircraft operating above 18,000 feet MSL. Jet Routes start at 18,000 feet MSL and extend upward to 45,000 feet
MSL (altitudes above 18,000 feet are called “flight levels” and are described as FL450 for 45,000 feet MSL). Jet
Routes are designated with a “J” before the route number.

AUDIO PANEL
& CNS

Low Altitude Airways are drawn in gray (the same shade used for roads). High Altitude Airways are drawn
in green. When both types of airways are displayed, High Altitude Airways are drawn on top of Low Altitude
Airways.
When airways are selected for display on the map, the airway waypoints (VORs, NDBs and Intersections) are
also displayed.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Low Altitude
Airway
(Victor Airway)

AFCS
ADDITIONAL
FEATURES

High Altitude
Airway
(Jet Route)

APPENDICES

Figure 5-22 Airways on MFD Navigation Page

INDEX

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Flight Management
Airways may be displayed on the map at the pilot’s discretion using either a combination of AIRWAYS Softkey
presses, or menu selections using the MENU Key from the Navigation Map Page. The Airway range can also be
programmed to only display Airways on the MFD when the map range is at or below a specific number.

FLIGHT
INSTRUMENTS

Displaying/removing airways:
1) Select the MAP Softkey.
2) Select the AIRWAYS Softkey. Both High and Low Altitude Airways are displayed (AIRWY ON).
3) Select the softkey again to display Low Altitude Airways only (AIRWY LO).

EIS

4) Select the softkey again to display High Altitude Airways only (AIRWY HI).
5) Select the softkey again to remove High Altitude Airways. No airways are displayed (AIRWAYS).
Or:
AUDIO PANEL
& CNS

1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key.

FLIGHT
MANAGEMENT

4) Turn the large FMS Knob to highlight the ‘AIRWAYS’ field.
5) Turn the FMS Knob to select ‘Off’, ‘All’, ‘LO Only’, or ‘HI Only’, and press the ENT Key.

HAZARD
AVOIDANCE

6) Press the FMS Knob to return to the Navigation Map Page.

Airway Display Selection

Off, All, LO Only, HI Only

Low Altitude Airway Range
High Altitude Airway Range

AFCS

Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup

The airway range is the maximum map range on which airways are displayed.

ADDITIONAL
FEATURES

Selecting an airway range (LOW ALT AIRWAY or HI ALT AIRWAY):
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Airway’ group.

APPENDICES

4) Press the ENT Key.
5) Highlight the ‘LOW ALT AIRWAY’ or ‘HI ALT AIRWAY’ range field.
6) To change the range setting, turn the small FMS Knob to display the range list.
7) Select the desired range using the small FMS Knob.

INDEX

8) Press the ENT Key.
9) Press the FMS Knob to return to the Navigation Map Page.

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SYSTEM
OVERVIEW

The following range items are configurable on the airways menu:
Airway Type

Symbol

Low Altitude Airway (LOW ALT AIRWAY)

300

High Altitude Airway (HI ALT AIRWAY)

FLIGHT
INSTRUMENTS

Default
Maximum
Range (nm) Range (nm)
200
500
500

Table 5-4 Airway Range Information
EIS

Track Vector

AUDIO PANEL
& CNS

The Navigation Map can display a track vector that is useful in minimizing track angle error. The track vector
is a solid light blue line segment extended to a predicted location. The track vector look-ahead time is selectable
(30 sec, 60 sec (default), 2 min, 5 min, 10 min, 20 min) and determines the length of the track vector. The track
vector shows up to 90 degrees of a turn for the 30 and 60 second time settings.
Track Vector

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 5-24 Navigation Map -Track Vector

Displaying/removing the track vector:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.

AFCS

2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
4) Press the ENT Key.

ADDITIONAL
FEATURES

5) Highlight the ‘TRACK VECTOR’ field.
6) Select ‘On’ or ‘Off’. Press the ENT Key to accept the selected option. The flashing cursor highlights the look
ahead time field. Use the FMS Knob to select the desired time. Press the ENT Key.
7) Press the FMS Knob to return to the Navigation Map Page.

APPENDICES
INDEX

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FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Flight Management

Wind Vector On/Off

EIS

Nav Range Ring On/Off

Track Vector
- On/Off
- Look Ahead Time

AUDIO PANEL
& CNS

Fuel Range
- On/Off
- Fuel Reserve Time
Figure 5-25 Navigation Map Setup Menu -TRACK VECTOR, WIND VECTOR, NAV RANGE RING, FUEL RANGE RING Setup

Wind Vector

FLIGHT
MANAGEMENT

The map displays a wind vector arrow in the upper right-hand portion of the screen. Wind vector information
is displayed as a white arrow pointing in the direction in which the wind is moving for wind speeds greater than
or equal to 1 kt.
Wind Direction

HAZARD
AVOIDANCE

Wind Speed
Figure 5-26 Navigation Map - Wind Vector

Note: The wind vector is not displayed until the aircraft is moving. It is not displayed on the Waypoint
AFCS

Information pages.
Displaying/removing the wind vector:

ADDITIONAL
FEATURES

1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.

APPENDICES

4) Press the ENT Key.
5) Highlight the ‘WIND VECTOR’ field.
6) Select ‘On’ or ‘Off’.

INDEX

7) Press the FMS Knob to return to the Navigation Map Page.

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SYSTEM
OVERVIEW

Nav Range Ring
The Nav Range Ring shows the direction of travel (ground track) on a rotating compass card. The range is
determined by the map range. The range is 1/4 of the map range (e.g., 37.5 nm on a 150 nm map).

FLIGHT
INSTRUMENTS

Range (radius)

EIS
AUDIO PANEL
& CNS

Nav Range Ring

FLIGHT
MANAGEMENT

Figure 5-27 Navigation Map - Nav Range Ring

HAZARD
AVOIDANCE

Note: The Nav Range Ring is not displayed on the Waypoint Information pages, Nearest pages, or Direct-to

Window map.
Displaying/removing the Nav Range Ring:

AFCS

1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.

ADDITIONAL
FEATURES

3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘NAV RANGE RING’ field.
6) Select ‘On’ or ‘Off’.

APPENDICES

7) Press the FMS Knob to return to the Navigation Map Page.
Note: The Nav Range Ring is referenced to either magnetic or true north, based on the selection on the AUX

- System Setup Page.

INDEX

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OVERVIEW

Flight Management

Fuel Range Ring

FLIGHT
INSTRUMENTS

The map can display a fuel range ring which shows the remaining flight distance. A dashed green circle
indicates the selected range to reserve fuel. A solid green circle indicates the total endurance range. If only
reserve fuel remains, the range is indicated by a solid yellow circle.

Total Endurance Range

AUDIO PANEL
& CNS

EIS

Time to Reserve Fuel

FLIGHT
MANAGEMENT

Range to Reserve Fuel

HAZARD
AVOIDANCE

Figure 5-28 Navigation Map - Fuel Range Ring

Displaying/removing the fuel range ring and selecting a fuel range time:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.

AFCS

2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
4) Press the ENT Key.
ADDITIONAL
FEATURES

5) Highlight the ‘FUEL RNG (RSV)’ field.
6) Select ‘On’ or ‘Off’.
7) Highlight the fuel reserve time field. This time should be set to the amount of flight time equal to the amount
of fuel reserve desired.

APPENDICES

8) To change the reserve fuel time, enter a time (00:00 to 23:59; hours:minutes). The default setting is 00:45
minutes.
9) Press the ENT Key.

INDEX

10) Press the FMS Knob to return to the Navigation Map Page.

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Flight Management
SYSTEM
OVERVIEW

Field of View (SVS)

FLIGHT
INSTRUMENTS

The map can display the boundaries of the PFD Synthetic Vision System (SVS) lateral field of view. The field
of view is shown as two dashed lines forming a V shape in front of the aircraft symbol on the map. This is only
available if SVS is installed on the aircraft.

EIS

Lateral Field
of View
Boundaries

AUDIO PANEL
& CNS

Figure 5-29 Navigation Map - Field of View

FLIGHT
MANAGEMENT

Displaying/removing the field of view:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.

HAZARD
AVOIDANCE

3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘FIELD OF VIEW’ field.
6) Select ‘On’ or ‘Off’.

AFCS

7) Press the ENT Key.
8) Press the FMS Knob to return to the Navigation Map Page.

ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

Flight Management

5.3 Waypoints

FLIGHT
INSTRUMENTS

Waypoints are predetermined geographical positions (internal database) or pilot-entered positions, and are
used for all phases of flight planning and navigation.
Communication and navigation frequencies can be tuned “automatically” from various Waypoint Information
(WPT) pages, Nearest (NRST) pages, and the Nearest Airports Window (on PFD). This auto-tuning feature
simplifies frequency entry over manual tuning. Refer to the CNS and Audio Panel section for details on autotuning.

AUDIO PANEL
& CNS

EIS

Waypoints can be selected by entering the ICAO identifier, entering the name of the facility, or by entering
the city name. See the System Overview section for detailed instructions on entering data in the G1000. As a
waypoint identifier, facility name, or location is entered, the G1000’s Spell’N’Find™ feature scrolls through the
database, displaying those waypoints matching the characters which have been entered to that point. A direct-to
navigation leg to the selected waypoint can be initiated by pressing the Direct-to Key on any of the waypoint
pages.
Identifier Entry Field

FLIGHT
MANAGEMENT

City Entry Field

Facility
Entry Field

Entered Waypoint on
Map

Map Area Showing
Entered Waypoint

HAZARD
AVOIDANCE

- Waypoint Identifier
- Type (symbol)
- Facility Name
- City

ADDITIONAL
FEATURES

AFCS

Waypoint Location

APPENDICES

Figure 5-30 Waypoint Information Window

INDEX

If duplicate entries exist for the entered facility name or location, additional entries may be viewed by continuing
to turn the small FMS Knob during the selection process. If duplicate entries exist for an identifier, a Duplicate
Waypoints Window is displayed when the ENT Key is pressed.

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Flight Management
SYSTEM
OVERVIEW

Identifier with
Duplicates

FLIGHT
INSTRUMENTS

Duplicate
Waypoints

EIS
AUDIO PANEL
& CNS

Duplicate Message

FLIGHT
MANAGEMENT

Airports

Figure 5-31 Waypoint Information Window - Duplicate Identifier

HAZARD
AVOIDANCE

Note: ‘North Up’ orientation on the Airport Information Page cannot be changed; the pilot needs to be

aware of proper orientation if the Navigation Map orientation is different from the Airport Information Page
Map.

AFCS

The Airport Information Page is the first page in WPT group and allows the pilot to view airport information,
load frequencies (COM, NAV, and lighting), review runways, and review instrument procedures that may be
involved in the flight plan. See the Audio Panel and CNS Section for more information on loading frequencies
(auto-tuning). After engine startup, the Airport Information Page defaults to the airport where the aircraft is
located. After a flight plan has been loaded, it defaults to the destination airport. On a flight plan with multiple
airports, it defaults to the airport which is the current active waypoint.

ADDITIONAL
FEATURES

In addition to displaying a map of the currently selected airport and surrounding area, the Airport Information
Page displays airport information in three boxes labeled ‘AIRPORT’, ‘RUNWAYS’, and ‘FREQUENCIES’. For
airports with multiple runways, information for each runway is available.

APPENDICES
INDEX

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OVERVIEW

Flight Management

Airport Information

- ID/Facility/City
- Usage Type/Region
- Lat/Long/Elev
- Fuel Available
- Time Zone (UTC Offset)

FLIGHT
INSTRUMENTS

Navigation Map
Showing Selected
Airport

Runway Information

EIS

- Designation
- Length/Width/Surface
- Lighting Available

COM/NAV Freq. Info.

Airport/Runway
Diagram
AUDIO PANEL
& CNS

- Identification
- Frequency
- Availability
- Additional Information

FLIGHT
MANAGEMENT

Softkeys
Figure 5-32 Airport Information Page

The following descriptions and abbreviations are used on the Airport Information Page:

HAZARD
AVOIDANCE

• Usage type: Public, Military, or Private
• Runway surface type: Hard, Turf, Sealed, Gravel, Dirt, Soft, Unknown, or Water
• Runway lighting type: No Lights, Part Time, Full Time, Unknown, or PCL Freq (for pilot-controlled
lighting)

AFCS

• COM Availability: TX (transmit only), RX (receive only), PT (part time), i (additional information available)
Selecting an airport for review by identifier, facility name, or location:
1) From the Airport Information Page, press the FMS Knob.
ADDITIONAL
FEATURES

2) Use the FMS Knobs and enter an identifier, facility name, or location.
3) Press the ENT Key.
4) Press the FMS Knob to remove the cursor.

APPENDICES

Selecting a runway:
1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to place the cursor in the ‘RUNWAYS’ Box, on the runway designator.
3) Turn the small FMS Knob to display the desired runway (if more than one) for the selected airport.

INDEX

4) To remove the flashing cursor, press the FMS Knob.

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SYSTEM
OVERVIEW

View a destination airport:
From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination
Airport is displayed.

Navigation Frequencies
ILS
LOC

EIS
AUDIO PANEL
& CNS

Communication Frequencies
Approach * Control
Pre-Taxi
Arrival *
CTA *
Radar
ASOS
Departure * Ramp
ATIS
Gate
Terminal *
AWOS
Ground
TMA *
Center
Helicopter
Tower
Class B *
Multicom
TRSA *
Class C *
Other
Unicom
Clearance

FLIGHT
INSTRUMENTS

The Airport Frequencies Box uses the descriptions and abbreviations listed in the following table:

FLIGHT
MANAGEMENT

* May include Additional Information
Table 5-5 Airport Frequency Abbreviations

HAZARD
AVOIDANCE

A departure, arrival, or approach can be loaded using the softkeys on the Airport Information Page. See the
procedures section for details. METARs or TAFs applicable to the selected airport can be selected for display (see
the Hazard Avoidance section for details about weather.
The G1000 provides a NRST Softkey on the PFD, which gives the pilot quick access to nearest airport
information (very useful if an immediate need to land is required). The Nearest Airports Window displays a
list of the 25 nearest airports (three entries can be displayed at one time). If there are more than three they are
displayed in a scrollable list. If there are no nearest airports available, “NONE WITHIN 200NM” is displayed.

Airport Identifier/
Type

AFCS

Bearing/Distance to Airport

Approach Available
ADDITIONAL
FEATURES

Length of Longest
Runway

COM Freq. Info.

- Identification
- Frequency

APPENDICES

Additional Airports
(within 200 nm)

INDEX

NRST Softkey
Figure 5-33 Nearest Airports Window on PFD

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SYSTEM
OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

Pressing the ENT Key displays the PFD Airport Information Window for the highlighted airport. Pressing the
ENT Key again returns to the Nearest Airports Window with the cursor on the next airport in the list. Continued
presses of the ENT Key sequences through the information pages for all airports in the Nearest Airports list.

Airport Information
- ID/Type/City
- Facility

EIS

Airport Information
- Usage/Time/Elev
- Region

Airport Information

AUDIO PANEL
& CNS

- Lat/Long

FLIGHT
MANAGEMENT

Figure 5-34 Airport Information Window on PFD

HAZARD
AVOIDANCE

The Nearest Airports Page on the MFD is first in the group of NRST pages because of its potential use in
the event of an in-flight emergency. In addition to displaying a map of the currently selected airport and
surrounding area, the page displays nearest airport information in five boxes labeled ‘NEAREST AIRPORTS’,
‘INFORMATION’, ‘RUNWAYS’, ‘FREQUENCIES’, and ‘APPROACHES’.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

The selected airport is indicated by a white arrow, and a dashed white line is drawn on the navigation map
from the aircraft position to the nearest airport. Up to five nearest airports, one runway, up to five frequencies,
and up to five approaches are visible at one time. If there are more than can be shown, each list can be scrolled.
If there are no items for display in a boxed area, text indicating that fact is displayed. The currently selected
airport remains in the list until it is unselected.

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SYSTEM
OVERVIEW

Nearest Airports

- ID/Type
- Bearing/Distance

FLIGHT
INSTRUMENTS

Airport Information

- Facility/City/Elevation

Runway Information

Nearest Airport

- Designation/Surface
- Length/Width

EIS

COM/NAV Freq. Info.
- Identification
- Frequency

Navigation Map
Showing Nearest
Airport

Window Selection
Softkeys

AUDIO PANEL
& CNS

Approaches Available

FLIGHT
MANAGEMENT

LD APR Softkey (only
available if an approach is
highlighted)
Figure 5-35 Nearest Airport Page

Viewing information for a nearest airport on the PFD:

HAZARD
AVOIDANCE

1) Press the NRST Softkey to display the Nearest Airports Window.
2) Highlight the airport identifier with the FMS Knob and press the ENT Key to display the Airport Information
Window.

AFCS

3) To return to the Nearest Airports Window press the ENT Key (with the cursor on ‘BACK’) or press the CLR
Key. The cursor is now on the next airport in the nearest airports list. (Repeatedly pressing the ENT Key
moves through the airport list, alternating between the Nearest Airports Window and the Airport Information
Window.)
4) Press the CLR Key to close the PFD Nearest Airports Window.

ADDITIONAL
FEATURES

Viewing information for a nearest airport on the MFD:
1) Turn the large FMS Knob to select the NRST page group.
2) Turn the small FMS Knob to select the Nearest Airports Page (it is the first page of the group, so it may already
be selected. If there are no Nearest Airports available, “NONE WITHIN 200 NM” is displayed.

APPENDICES

3) Press the APT Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Airport Window’ and
press the ENT Key. The cursor is placed in the ‘NEAREST AIRPORTS’ Box. The first airport in the nearest airports
list is highlighted.
4) Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also moves to the next airport)

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INDEX

5) Press the FMS Knob to remove the flashing cursor.

165

SYSTEM
OVERVIEW

Viewing runway information for a specific airport:

FLIGHT
INSTRUMENTS

Flight Management

2) Turn the small FMS Knob to select the desired runway.

1) With the Nearest Airports Page displayed, press the RNWY Softkey; or press the MENU Key, highlight ‘Select
Runway Window’; and press the ENT Key. The cursor is placed in the ‘RUNWAYS’ Box.
3) Press the FMS Knob to remove the flashing cursor.

See the Audio Panel and CNS Section for frequency selection and the Procedures section for approaches.

EIS

The Nearest Airports Box on the System Setup Page defines the minimum runway length and surface type
used when determining the 25 nearest airports to display on the MFD Nearest Airports Page. A minimum
runway length and/or surface type can be entered to prevent airports with small runways or runways that are
not appropriately surfaced from being displayed. Default settings are 0 feet (or meters) for runway length and
“HARD/SOFT” for runway surface type.

AUDIO PANEL
& CNS

Selecting nearest airport surface matching criteria:
1) Use the FMS Knob to select the System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.

FLIGHT
MANAGEMENT

3) Turn the large FMS Knob to highlight the runway surface field in the Nearest Airports Box.
4) Turn the small FMS Knob to select the desired runway option (ANY, HARD ONLY, HARD/SOFT).
5) Press the ENT Key.

HAZARD
AVOIDANCE

Selecting nearest airport minimum runway length matching criteria:
1) Use the FMS Knob to select the System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the minimum length field in the Nearest Airport Box.

APPENDICES

ADDITIONAL
FEATURES

AFCS

4) Use the FMS Knob to enter the minimum runway length (zero to 25,000 feet) and press the ENT Key.

Nearest Airport Criteria

- Type of Runway Surface
- Minimum Runway Length

INDEX

Figure 5-36 System Setup Page - Nearest Airport Selection Criteria

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Flight Management
SYSTEM
OVERVIEW

Intersections
Note: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR

FLIGHT
INSTRUMENTS

used to define the intersection.
The Intersection Information Page is used to view information about intersections. In addition to displaying
a map of the currently selected intersection and surrounding area, the Intersection Information Page displays
intersection information in three boxes labeled ‘INTERSECTION’, ‘INFORMATION’, and ‘NEAREST VOR’.

Navigation Map
Showing Selected
Intersection

EIS

Intersection Identifier
Intersection Info

AUDIO PANEL
& CNS

- Region
- Lat/Long

Nearest VOR Info

- Identifier/Type (symbol)
- Radial to VOR
- Distance to VOR

Selected Intersection

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 5-37 Intersection Information Page

AFCS

Select an intersection:
1) With the Intersection Information Page displayed, enter an identifier in the Intersection Box.
2) Press the ENT Key.

ADDITIONAL
FEATURES

3) Press the FMS Knob to remove the flashing cursor.

Or:

1) With the Nearest Intersections Page displayed, press the FMS Knob

APPENDICES

2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest Intersection Box.
3) Press the FMS Knob to remove the flashing cursor.

The Nearest Intersections Page can be used to quickly find an intersection close to the flight path. In addition
to displaying a map of the surrounding area, the page displays information for up to 25 nearest intersections in
three boxes labeled ‘NEAREST INT’, ‘INFORMATION’, and ‘REFERENCE VOR’.

INDEX

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OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

The selected intersection is indicated by a white arrow. Up to eleven intersections are visible at a time. If
there are more than can be shown, the list can be scrolled. If there are no items for display, text indicating that
fact is displayed
Note: The list only includes waypoints that are within 200 nm.

Intersection Information
- Identifier/Symbol
- Bearing/Distance to
intersection from
aircraft position

AUDIO PANEL
& CNS

EIS

Navigation Map
Showing Nearest
Intersection

Intersection Lat/Long

FLIGHT
MANAGEMENT

Reference VOR Info

- Identifier/Type (symbol)
- VOR Frequency
- Bearing/Distance to VOR

HAZARD
AVOIDANCE

Nearest
Intersection

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 5-38 Nearest Intersections Page

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Flight Management
SYSTEM
OVERVIEW

NDBs

FLIGHT
INSTRUMENTS

The NDB Information Page is used to view information about NDBs. In addition to displaying a map of
the currently selected NDB and surrounding area, the page displays NDB information in four boxes labeled
‘NDB’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT.
NDB Identifier/Type
- Facility Name
- Nearest City

Navigation Map
Showing Selected
NDB

NDB Information

EIS

- Type
- Region
- Lat/Long

AUDIO PANEL
& CNS

NDB Frequency

Selected NDB

Nearest Airport Info

- Identifier/Type (symbol)
- Bearing/Distance to
Airport

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 5-39 NDB Information Page

Note: Compass locator (LOM): a low power, low or medium frequency radio beacon installed in conjunction

with the instrument landing system. When LOM is used, the locator is at the Outer Marker; when LMM is
used, the locator is at the Middle Marker.
AFCS

Select an NDB:

ADDITIONAL
FEATURES

1) With the NDB Information Page displayed, enter an identifier, the name of the NDB, or the city in which it’s
located in the NDB Box.
2) Press the ENT Key.
3) Press the FMS Knob to remove the flashing cursor.

Or:
APPENDICES

1) With the Nearest NDB Page displayed, press the FMS Knob
2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest NDB Box.
3) Press the FMS Knob to remove the flashing cursor.

INDEX

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Flight Management
The Nearest NDB Page can be used to quickly find a NDB close to the flight path. In addition to displaying
a map of the surrounding area, the page displays information for up to 25 nearest NDBs in three boxes labeled
‘NEAREST NDB’, ‘INFORMATION’, and ‘FREQUENCY’.

FLIGHT
INSTRUMENTS

A white arrow before the NDB identifier indicates the selected NDB. Up to eleven NDBs are visible at a time.
If there are more than can be shown, each list can be scrolled. The list only includes waypoints that are within
200nm. If there are no NDBs in the list, text indicating that there are no nearest NDBs is displayed. If there are
no nearest NDBs in the list, the information and frequency fields are dashed.

NDB Identifier/Symbol
- Bearing/Distance to
NDB from aircraft
position

AUDIO PANEL
& CNS

EIS

Navigation Map
Showing Selected
NDB

Nearest NDB
FLIGHT
MANAGEMENT

NDB Information

- Facility Name/City
- Type
- Lat/Long

HAZARD
AVOIDANCE

NDB Frequency

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 5-40 Nearest NDB Page

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Flight Management
SYSTEM
OVERVIEW

VORs

FLIGHT
INSTRUMENTS

The VOR Information Page can be used to view information about VOR and ILS signals (since ILS signals
can be received on a NAV receiver), or to quickly auto-tune a VOR or ILS frequency. Localizer information
cannot be viewed on the VOR Information Page. If a VOR station is combined with a TACAN station it is
listed as a VORTAC on the VOR Information Page and if it includes only DME, it’s displayed as VOR-DME.
In addition to displaying a map of the currently selected VOR and surrounding area, the VOR Information
Page displays VOR information in four boxes labeled ‘VOR’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST
AIRPORT’.

EIS

VOR Identifier/Type
- Facility Name
- Nearest City

AUDIO PANEL
& CNS

Navigation Map
Showing
Selected VOR

VOR Information

- Class/Magnetic Variation
- Region
- Lat/Long

FLIGHT
MANAGEMENT

VOR Frequency

Selected VOR

Nearest Airport Info

- Identifier/Type (symbol)
- Bearing/Distance to
Airport

HAZARD
AVOIDANCE

Figure 5-41 VOR Information Page
AFCS

The VOR classes used in the VOR information box are: LOW ALTITUDE, HIGH ALTITUDE, and
TERMINAL
Select a VOR:

ADDITIONAL
FEATURES

1) With the VOR Information Page displayed, enter an identifier, the name of the VOR, or the city in which it’s
located in the VOR Box.
2) Press the ENT Key.

APPENDICES

3) Press the FMS Knob to remove the flashing cursor.
Or:

1) With the Nearest VOR Page displayed, press the FMS Knob or press the VOR Softkey.
2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box.

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INDEX

3) Press the FMS Knob to remove the flashing cursor.
Or:

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171

SYSTEM
OVERVIEW

Flight Management
1) With the Nearest VOR Page displayed, press the MENU Key.
2) Highlight ‘SELECT VOR WINDOW’, and press the ENT Key.

FLIGHT
INSTRUMENTS

3) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box.
4) Press the FMS Knob to remove the flashing cursor.

EIS

The Nearest VOR Page can be used to quickly find a VOR station close to the aircraft. Also, a NAV frequency
from a selected VOR station can be loaded from the Nearest VOR Page. In addition to displaying a map of
the surrounding area, the Nearest VOR Page displays information for up to 25 nearest VOR stations in three
boxes labeled ‘NEAREST VOR’, ‘INFORMATION’, and ‘FREQUENCY’. The list only includes waypoints that
are within 200 nm.

AUDIO PANEL
& CNS

A white arrow before the VOR identifier indicates the selected VOR. Up to eleven VORs are visible at a
time. If there are more than can be shown, each list can be scrolled. If there are no VORs in the list, text
indicating that there are no nearest VORs is displayed. If there are no nearest VORs in the list, the information
is dashed.

VOR Identifier/Symbol

- Bearing/Distance to VOR
from aircraft position

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Navigation Map
Showing Nearest
VOR

VOR Information

AFCS

- Facility Name/City
- Class/Magnetic Variation
- Lat/Long

VOR Frequency

ADDITIONAL
FEATURES

Nearest VOR

INDEX

APPENDICES

Figure 5-42 Nearest VOR Page

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Flight Management
SYSTEM
OVERVIEW

User Waypoints

FLIGHT
INSTRUMENTS

The G1000 can create and store up to 1,000 user-defined waypoints. User waypoints can be created from
any map page (except PFD Inset Map, AUX-Trip Planning Page, or Procedure Pages) by selecting a position on
the map using the Joystick, or from the User Waypoint Information Page by referencing a bearing/distance
from an existing waypoint or bearing from two existing waypoints. Once a waypoint has been created, it can
be renamed, deleted, or moved.

User Waypoint Info
User Wpt Comment
Navigation Map
Showing Selected
User Waypoint

Reference Wpt/Info

Selected User
Waypoint

User Waypoint List

EIS

- Identifier
- Temporary/Normal
- Waypoint Type

AUDIO PANEL
& CNS

- Identifier/Rad/Dist or
- Identifiers/Radials or
- Region/Lat/Long
- Identifier
- Comment

FLIGHT
MANAGEMENT

# User Wpts Used

Figure 5-43 User Waypoint Information Page

HAZARD
AVOIDANCE

Softkeys

GO BACK Softkey
displayed if User Wpt
was created on map
page

AFCS

Select a User Waypoint:
1) With the User Waypoint Information Page displayed, enter the name of the User Waypoint, or scroll to the
desired waypoint in the User Waypoint List using the large FMS Knob.

ADDITIONAL
FEATURES

2) Press the ENT Key.
3) Press the FMS Knob to remove the flashing cursor.

Or:

1) With the Nearest User Waypoint Page displayed, press the FMS Knob
APPENDICES

2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest USR Box.
3) Press the FMS Knob to remove the flashing cursor.

INDEX

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OVERVIEW

Flight Management

Nearest User Wpt List

- Identifier
- Bearing/Distance from
aircraft position

FLIGHT
INSTRUMENTS

Navigation Map
Showing Selected
User Waypoint

EIS

User Waypoint Info
- Comment
- Lat/Long

Reference Wpt Info

AUDIO PANEL
& CNS

Selected User
Waypoint

- Identifier
- Radial/Distance

FLIGHT
MANAGEMENT

Figure 5-44 Nearest User Waypoint Page

Creating User Waypoints
User waypoints can be created from the User Waypoint Information Page in the following ways:

HAZARD
AVOIDANCE

Creating user waypoints from the User Waypoint Information Page:
1) Select the NEW Softkey, or press the MENU Key and select ‘Create New User Waypoint’.
2) Enter a user waypoint name (up to six characters).
3) Press the ENT Key. The current aircraft position is the default location of the new waypoint.

APPENDICES

ADDITIONAL
FEATURES

AFCS

4) If desired, define the type and location of the waypoint in one of the following ways:

a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint
identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.

Or:

b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier,
the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs.

Or:

c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into
the INFORMATION window using the FMS Knobs.

5) Press the ENT Key to accept the new waypoint.

INDEX

6) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor
to “TEMPORARY” and selecting the ENT Key to check or uncheck the box.
7) Press the FMS Knob to remove the flashing cursor.

174

Or:

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Flight Management
SYSTEM
OVERVIEW

1) Press the FMS Knob to activate the cursor.
2) Enter a user waypoint name (up to six characters).

FLIGHT
INSTRUMENTS

3) Press the ENT Key. The message ‘Are you sure you want to create the new User Waypoint AAAAAA?’ is
displayed.
4) With ‘YES’ highlighted, press the ENT Key.
5) If desired, define the type and location of the waypoint in one of the following ways:
a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint
identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.

Or:

b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier,
the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs.

Or:

c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into
the INFORMATION window using the FMS Knobs.

EIS

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

6) Press the ENT Key to accept the new waypoint.
7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor
to “TEMPORARY” and selecting the ENT Key to check or uncheck the box.
8) Press the FMS Knob to remove the flashing cursor.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Figure 5-45 User Waypoint Information Page Menu

APPENDICES

Creating user waypoints from map pages:
1) Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint.
2) Press the ENT Key. The User Waypoint Information Page is displayed with the captured position.

INDEX

Note: If the pointer has highlighted a map database feature, one of three things happens upon pressing

the ENT Key: 1) information about the selected feature is displayed instead of initiating a new waypoint,
2) a menu pops up allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or 3) a new
waypoint is initiated with the default name being the selected map item.
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SYSTEM
OVERVIEW

Flight Management
3) Enter a user waypoint name (up to six characters).
4) Press the ENT Key to accept the selected name. The first reference waypoint box is highlighted.

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

5) If desired, define the type and location of the waypoint in one of the following ways:

a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint
identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.

Or:

b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier,
the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs.

Or:

c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into
the INFORMATION window using the FMS Knobs.

FLIGHT
MANAGEMENT

8) Press the FMS Knob to remove the flashing cursor.
9) Press the GO BACK Softkey to return to the map page.

Editing User Waypoints

HAZARD
AVOIDANCE

Editing a user waypoint comment or location:
1) With the User Waypoint Information Page displayed, press the FMS Knob to activate the cursor.
2) Move the cursor to the desired field.
3) Turn the small FMS Knob to make any changes.

AFCS

4) Press the ENT Key to accept the changes.
5) Press the FMS Knob to remove the flashing cursor.

ADDITIONAL
FEATURES

Renaming user waypoints:
1) Highlight a user waypoint in the User Waypoint List. Press the RENAME Softkey, or press the MENU Key and
select ‘Rename User Waypoint’
2) Enter a new name.

APPENDICES

3) Press the ENT Key. The message ‘Do you want to rename the user waypoint AAAAAA to BBBBBB?’ is
displayed.
4) With ‘YES’ highlighted, press the ENT Key.

INDEX

5) Press the FMS Knob to remove the flashing cursor.

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SYSTEM
OVERVIEW

Changing the location of an existing waypoint to the aircraft present position:
1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key.
2) Press the MENU Key.

FLIGHT
INSTRUMENTS

3) Select ‘Use Present Position’.
4) Press the ENT Key twice. The new waypoint’s location is saved.
5) Press the FMS Knob to remove the flashing cursor.

EIS

A system generated comment for a user waypoint incorporates the reference waypoint identifier, bearing,
and distance. If a system generated comment has been edited, a new comment can be generated.
Resetting the comment field to the system generated comment:
1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key.

AUDIO PANEL
& CNS

2) Press the MENU Key.
3) Select ‘Auto Comment’.
4) Press the ENT Key. The generated comment is based on the reference point used to define the waypoint.

FLIGHT
MANAGEMENT

The default type of user waypoint (normal or temporary) can be changed using the user waypoint information
page menu. Temporary user waypoints are automatically deleted upon the next power cycle.
Changing the user waypoint storage duration default setting:
1) With the User Waypoint Information Page displayed, press the MENU Key.

HAZARD
AVOIDANCE

2) Move the cursor to select ‘Waypoint Setup’, and press the ENT Key.
3) Select ‘NORMAL’ or ‘TEMPORARY’ as desired, and press the ENT Key
4) Press the FMS Knob to remove the flashing cursor and return to the User Waypoint Information Page.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Flight Management
Deleting User Waypoints
Deleting a single user waypoint

FLIGHT
INSTRUMENTS

1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field.
2) Press the DELETE Softkey or press the CLR Key. ‘Yes’ is highlighted in the confirmation window.
3) Press the ENT Key.
4) Press the FMS Knob to remove the flashing cursor.

Or:

EIS

1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field.
2) Press the MENU Key.

AUDIO PANEL
& CNS

3) Select ‘Delete User Waypoint’.
4) Press the ENT Key twice to confirm the selection.
5) Press the FMS Knob to remove the flashing cursor.

FLIGHT
MANAGEMENT

Deleting all user waypoints
1) Highlight a User Waypoint in the User Waypoint List.
2) Press the MENU Key.
3) Select ‘Delete All User Waypoints’

HAZARD
AVOIDANCE

4) Press the ENT Key twice to confirm the selection.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

5) Press the FMS Knob to remove the flashing cursor.

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OVERVIEW

5.4 Airspaces

FLIGHT
INSTRUMENTS

The G1000 can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA
(Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and Temporary Flight Restriction (TFR).

Class D Airspace
EIS

MOA (Military)

Class B Airspace

Restricted Area
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Alert Area

Class C Airspace

AFCS
ADDITIONAL
FEATURES

ADIZ
Warning Area

APPENDICES

Figure 5-46 Airspaces

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The Nearest Airspaces Page, Airspace Alerts Window, and Airspace Alerts on the PFD provide additional
information about airspaces and the location of the aircraft in relationship to them.

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FLIGHT
INSTRUMENTS

The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off.
This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the
Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an
airspace.
An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For example,
if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an alert message is
not generated, but if the aircraft is less than 500 feet above/below an airspace and projected to enter it, the pilot
is notified with an alert message. The default setting for the altitude buffer is 200 feet.

EIS

Changing the altitude buffer distance setting:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
AUDIO PANEL
& CNS

3) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box.
4) Use the FMS Knob to enter an altitude buffer value and press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.

FLIGHT
MANAGEMENT

Turning an airspace alert on or off:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box.

HAZARD
AVOIDANCE

4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF.

AFCS

5) Press the FMS Knob to remove the flashing cursor.

Airspace Alerts Box

APPENDICES

ADDITIONAL
FEATURES

- Airspace Altitude Buffer
- Alert On/Off
(Default Settings Shown)

INDEX

DFLTS Softkey
Figure 5-47 System Setup Page - Airspace Alerts

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OVERVIEW

Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup Menu. See Table
5-2 for the default and maximum ranges for each type of airspace and the symbol used to define the airspace
area.

FLIGHT
INSTRUMENTS

The Nearest Airspaces Page can be used to quickly find airspaces close to the flight path. In addition, a selected
frequency associated with the airspace can be loaded from the Nearest Airspaces Page. In addition to displaying
a map of airspace boundaries and surrounding area, the Nearest Airspaces Page displays airspace information in
four boxes labeled ‘AIRSPACE ALERTS’, ‘AIRSPACE, AGENCY’, VERTICAL LIMITS’, and ‘FREQUENCIES’.

EIS

Airspace Alerts Info

Airspace 1

AUDIO PANEL
& CNS

- Name
- Proximity (Ahead, Inside,
Ahead < 2nm, Within 2nm)
- Time till Intercept (only if
Ahead or Ahead < 2nm)

Airspace/Agency Info
- Airspace Type
- Controlling Agency

FLIGHT
MANAGEMENT

Airspace Vertical Limits
- Ceiling
- Floor

Airspace 2

Associated Frequencies

HAZARD
AVOIDANCE

- Type
- Availability/Info
- Frequency

Softkeys
Figure 5-48 Nearest Airspaces Page

AFCS

Airspace alerts and associated frequencies are shown in scrollable lists on the Nearest Airspaces Page. The
ALERTS and FREQ softkeys place the cursor in the respective list. The FREQ Softkey is enabled only if one or
more frequencies exist for a selected airspace.

ADDITIONAL
FEATURES

Selecting and viewing an airspace alert with its associated information:
1) Select the Nearest Airspace Page.
2) Press the ALERTS Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Alerts Window’,
and press the ENT Key. The cursor is placed in the ‘AIRSPACE ALERTS’ Box.

APPENDICES

3) Select the desired airspace.
4) Press the FMS Knob to remove the flashing cursor.

INDEX

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Pressing the PFD ALERTS Softkey displays the message window on the PFD. The following airspace alerts are
displayed in the message window:

EIS

FLIGHT
INSTRUMENTS

Message
INSIDE ARSPC – Inside airspace.
ARSPC AHEAD – Airspace ahead –
less than 10 minutes.
ARSPC NEAR – Airspace near and
ahead.
ARSPC NEAR – Airspace near –
less than 2 nm.

Comments
The aircraft is inside the airspace.
Special use airspace is ahead of aircraft. The aircraft penetrates the airspace within 10
minutes.
Special use airspace is near and ahead of the aircraft position.
Special use airspace is within 2 nm of the aircraft position.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Table 5-6 PFD Airspace Alert Messages

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OVERVIEW

5.5 Direct-to-Navigation

FLIGHT
INSTRUMENTS

The Direct-to method of navigation, initiated by pressing the Direct-to Key on either the MFD or PFD, is
quicker to use than a flight plan when the desire is to navigate to a single point such as a nearby airport.
Once a direct-to is activated, the G1000 establishes a point-to-point course line from the present position to the
selected direct-to destination. Course guidance is provided until the direct-to is replaced with a new direct-to or
flight plan, or cancelled.

EIS

A vertical navigation (VNV) direct-to creates a descent path (and provides guidance to stay on the path) from
the current altitude to a selected altitude at the direct-to waypoint. Vertical navigation is based on barometric
altitudes, not on GPS altitude, and is used for cruise and descent phases of flight.
The Direct-to Window allows selection and activation of direct-to navigation. The Direct-to Window displays
selected direct-to waypoint data on the PFD and the MFD.

AUDIO PANEL
& CNS

Direct-to Point Info
VNV Constraints

- Altitude at Arrival
- Along Track Offset

FLIGHT
MANAGEMENT

- Identifier/Symbol/Region
- Facility Name
- City

Map of Selected Point

HAZARD
AVOIDANCE

Location of Destination
- Bearing/Distance

AFCS

Desired Course
Figure 5-49 Direct-to Window - MFD

ADDITIONAL
FEATURES
APPENDICES
INDEX

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Direct-to Point Info

- Identifier/Symbol/City
- Facility Name

FLIGHT
INSTRUMENTS

VNV Constraints

- Altitude at Arrival
- Along Track Offset

Direct-to Point Info
- Bearing/Distance
- Desired Course

EIS

Activation Command

AUDIO PANEL
& CNS

Figure 5-50 Direct-to Window - PFD

Any waypoint can be entered as a direct-to destination from the Direct-to Window.
Entering a waypoint identifier, facility name, or city as a direct-to destination:

FLIGHT
MANAGEMENT

1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan wayoint as the default
selection or a blank waypoint field if no flight plan is active).

HAZARD
AVOIDANCE

2) Turn the small FMS Knob clockwise to begin entering a waypoint identifier (turning it counter-clockwise brings
up the waypoint selection submenu - press the CLR Key to remove it), or turn the large FMS Knob to select the
facility name, or city field and turn the small FMS Knob to begin entering a facility name or city. If duplicate
entries exist for the entered facility or city name, additional entries can be viewed by turning the small FMS
Knob during the selection process.
3) Press the ENT Key. The ‘Activate?’ field is highlighted.
4) Press the ENT Key to activate the direct-to.

AFCS

Any waypoint contained in the active flight plan can be selected as a direct-to waypoint from the Direct-to
Window, the Active Flight Plan Page, or the Active Flight Plan Window.
Waypoint Submenu

APPENDICES

ADDITIONAL
FEATURES

- Flight Plan Waypoints
- Nearest Waypoints
- Recent Waypoints
- User Waypoints
- Airway Waypoints
(only available when
active leg is part of an
airway)

INDEX

Figure 5-51 Waypoint Submenu

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Selecting an active flight plan waypoint as a direct-to destination:
1) While navigating an active flight plan, press the Direct-to Key. The Direct-to Window is displayed with the
active flight plan waypoint as the default selection.

FLIGHT
INSTRUMENTS

2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated
only when navigating a flight plan).
3) Select the desired waypoint.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
5) Press the ENT Key again to activate the direct-to.

EIS

Or:

1) Select the Active Flight Plan Page on the MFD, or the Active Flight Plan Window on the PFD.
AUDIO PANEL
& CNS

2) Select the desired waypoint.
3) Press the Direct-to Key.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.

FLIGHT
MANAGEMENT

5) Press the ENT Key again to activate the direct-to.

Any NRST, RECENT, USER, or AIRWAY waypoint can be selected as a direct-to destination in the Direct-to
Window.
Selecting a NRST, RECENT, USER, or AIRWAY waypoint as a direct-to destination:

HAZARD
AVOIDANCE

1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan destination as the
default selection or a blank destination if no flight plan is active).
2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated
only when navigating a flight plan).
3) Turn the small FMS Knob clockwise to display the NRST, RECENT, USER, or AIRWAY waypoints

AFCS

4) Turn the large FMS Knob clockwise to select the desired waypoint.
5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
6) Press the ENT Key again to activate the direct-to.

ADDITIONAL
FEATURES

The Direct-to Window can be displayed from any page and allows selection and activation of direct-to navigation.
If the direct-to is initiated from any page except the WPT pages, the default waypoint is the active flight plan
waypoint (if a flight plan is active) or a blank waypoint field. Direct-to requests on any WPT page defaults to the
displayed waypoint.

APPENDICES

Selecting any waypoint as a direct-to destination:
1) Select the page or window containing the desired waypoint type and select the desired waypoint.
2) Press the Direct-to Key to display the Direct-to Window with the selected waypoint as the direct-to
destination.

INDEX

3) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
4) Press ENT again to activate the direct-to.

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Selecting a nearby airport as a direct-to destination:
1) Press the NRST Softkey on the PFD; or turn the FMS Knob to display the Nearest Airports Page.

FLIGHT
INSTRUMENTS

2) Select the desired airport (the nearest one is already selected).
3) Press the Direct-to Key.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
5) Press the ENT Key again to activate the direct-to.

EIS

Direct-to destinations may also be selected by using the pointer on the navigation map pages. If no airport,
NAVAID, or user waypoint exists at the desired location, a temporary waypoint named ‘MAPWPT’ is automatically
created at the location of the map arrow.
Selecting a waypoint as a direct-to destination using the pointer:

AUDIO PANEL
& CNS

1) From a navigation map page, press the Joystick to display the pointer.
2) Move the Joystick to place the pointer at the desired destination location.
3) If the pointer is placed on an existing airport, NAVAID, or user waypoint, the waypoint name is highlighted.

FLIGHT
MANAGEMENT

4) Press the Direct-to Key to display the Direct-to Window with the selected point entered as the direct-to
destination.
5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
6) Press the ENT Key again to activate the direct-to.

HAZARD
AVOIDANCE

Cancelling a Direct-to:
1) Press the Direct-to Key to display the Direct-to Window.
2) Press the MENU Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is still active, the G1000 resumes
navigating the flight plan along the closest leg.

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OVERVIEW

Page Menu

FLIGHT
INSTRUMENTS

- Cancel Direct-To
Navigation

EIS
AUDIO PANEL
& CNS

Figure 5-52 Direct-to Window - Cancelling Direct-to Navigation
FLIGHT
MANAGEMENT

When navigating a direct-to, the G1000 sets a direct great circle course to the selected destination. The course
to a destination can also be manually selected using the course field (‘COURSE’) on the Direct-to Window.
Selecting a manual direct-to course:

HAZARD
AVOIDANCE

1) Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted.
2) Highlight the course field.
3) Enter the desired course.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.

AFCS

5) Press the ENT Key again to activate the direct-to.

Reselecting the direct course from the current position:
ADDITIONAL
FEATURES

1) Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted.
2) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
3) Press the ENT Key again to activate the direct-to.

APPENDICES

A direct-to with altitude constraints creates a descent path (and provides guidance to stay on the path) from the
aircraft’s current altitude to the altitude of the direct-to waypoint. The altitude is reached at the waypoint, or at the
specified distance along the flight path if an offset distance has been entered. All VNV altitudes prior to the directto destination are removed from the active flight plan upon successful activation of a direct-to destination that is
part of the active flight plan. All VNV altitudes following the direct-to waypoint are retained. See the section on
Vertical Navigation for more information regarding the use and purpose of VNV altitudes and offset distances.

INDEX

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Entering a VNV altitude and along-track offset for the waypoint:
1) Press the Direct-to Key to display the Direct-to Window.

FLIGHT
INSTRUMENTS

2) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
3) Enter the desired altitude.
4) Press the ENT Key. The option to select MSL or AGL is now displayed.
5) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
6) Press the ENT Key. The cursor is now flashing in the VNV offset distance field.
EIS

7) Enter the desired distance along-track before (-) or after (+) the offset waypoint.
8) Press the ENT Key. The ‘Activate?’ field is highlighted.

AUDIO PANEL
& CNS

9) Press the ENT Key to activate.

Removing a VNV altitude constraint:
1) Press the Direct-to Key to display the Direct-to Window.

FLIGHT
MANAGEMENT

2) Press the MENU Key.
3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key.

HAZARD
AVOIDANCE

Page Menu

ADDITIONAL
FEATURES

AFCS

- Clear Vertical Navigation
Constraints

INDEX

APPENDICES

Figure 5-53 Direct-to Window - Clearing Vertical Constraints

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5.6 Flight Planning

Flight Plan Leg Type

FLIGHT
INSTRUMENTS

Flight planning on the G1000 consists of building a flight plan by entering waypoints one at a time, adding
waypoints along airways, and inserting departures, airways, arrivals, or approaches as needed. The G1000 allows
flight planning information to be entered from either the MFD or PFD. The flight plan is displayed on maps using
different line widths, colors, and types, based on the type of leg and the segment of the flight plan currently being
flown (departure, enroute, arrival, approach, or missed approach).
Symbol

EIS

Active non-heading Leg
Active heading Leg

AUDIO PANEL
& CNS

Non-heading Leg in the current flight segment
Heading Leg not in the current flight segment

FLIGHT
MANAGEMENT

Non-heading leg not in the active flight segment
Turn Anticipation Arc

HAZARD
AVOIDANCE

Table 5-7 Flight Plan Leg Symbols

AFCS

Up to 99 flight plans with up to 99 waypoints each can be created and stored in memory. One flight plan can be
activated at a time and becomes the active flight plan. The active flight plan is erased when the system is turned
off and overwritten when another flight plan is activated. When storing flight plans with an approach, departure,
or arrival, the G1000 uses the waypoint information from the current database to define the waypoints. If the
database is changed or updated, the G1000 automatically updates the information if the procedure has not been
modified. If an approach, departure, or arrival procedure is no longer available, the procedure is deleted from the
affected stored flight plan(s), and an alert is displayed (see Miscellaneous System Messages) advising that one or
more stored flight plans need to be edited.

ADDITIONAL
FEATURES
APPENDICES

Whenever an approach, departure, or arrival procedure is loaded into the active flight plan, a set of approach,
departure, or arrival waypoints is inserted into the flight plan along with a header line describing the instrument
procedure the pilot selected. The original enroute portion of the flight plan remains active (unless an instrument
procedure is activated) when the procedure is loaded.

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When the database is updated, the airways need to be reloaded also. Each airway segment is reloaded from
the database given the entry waypoint, the airway identifier and the exit waypoint. This re-loads the sequence of
waypoints between the entry and exit waypoints (the sequence may change when the database is updated). The
update of an airway can fail during this process. If that happens, the airway waypoints are changed to regular
(non-airway) flight plan waypoints, and an alert is displayed (see Miscellaneous System Messages).

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SYSTEM
OVERVIEW

Flight Management
The following could cause the airway update to fail:
• Airway identifier, entry waypoint or exit waypoint not found in the new database.

FLIGHT
INSTRUMENTS

• Airway entry/exit waypoint is not an acceptable waypoint for the airway – either the waypoint is no longer on
the airway, or there is a new directional restriction that prevents it being used.
• Loading the new airway sequence would exceed the capacity of the flight plan.

Flight Plan Creation
There are three methods to create or modify a flight plan:

EIS

• Active Flight Plan Page on the MFD (create/modify the active flight plan)
• Active Flight Plan Window on the PFD (create/modify the active flight plan)

AUDIO PANEL
& CNS

• Flight Plan Catalog Page on the MFD (create/modify a stored flight plan)

FLIGHT
MANAGEMENT

Active FPL Waypoint List

- Comment
- Procedure Header
- Waypoint Identifier
- Airway Identifier
- Desired Track to Waypoint
- Distance to Waypoint
- Waypoint Altitude Constraint

HAZARD
AVOIDANCE

Active Flight
Plan Leg

Turn Anticipation
Arc

Vertical Navigation Profile
- Active Vertical WPT Alt/ID
- Vertical Speed Target
- Flight Path Angle
- Vertical Speed Target
- Time to Top of Descent
- Vertical Deviation

AFCS

Non-Active,
Flight Plan Leg

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 5-54 Active Flight Plan Page

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SYSTEM
OVERVIEW

Active Flight Plan Comment

FLIGHT
INSTRUMENTS

Active Flight
Plan Leg
Active Flight Plan Waypoint List
- Waypoint ID
- Desired Track to Waypoint
- Distance to Waypoint
- Airway Identifier

EIS

Figure 5-55 Active Flight Plan Window on PFD
AUDIO PANEL
& CNS

Catalog Contents
- # Used
- # Empty

FLIGHT
MANAGEMENT

Flight Plan List
- Comment

HAZARD
AVOIDANCE

Selected
Flight Plan
Map
Selected FPL Info

AFCS

- Departure Waypoint
- Destination Waypoint
- Total Flight Plan Distance
- Enroute Safe Altitude

Softkeys
Figure 5-56 Flight Plan Catalog Page

ADDITIONAL
FEATURES

The active flight plan is listed on the active Flight Plan Page on the MFD, and in the Active Flight Plan
Window on the PFD. It is the flight plan to which the G1000 is currently providing guidance, and is shown
on the navigation maps. Stored flight plans are listed on the Flight Plan Catalog Page, and are available for
activation (becomes the active flight plan).

APPENDICES

Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).

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3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a
waypoint selection submenu allowing selection of active flight plan, nearest, recent, or airway waypoints).

191

SYSTEM
OVERVIEW

Flight Management
4) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of
waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.

FLIGHT
INSTRUMENTS

6) When all waypoints have been entered, press the FMS Knob to remove the cursor.

Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.

EIS

3) Press the NEW Softkey; or press the MENU Key, highlight ‘Create New Flight Plan’, and press the ENT Key to
display a blank flight plan for the first empty storage location.

AUDIO PANEL
& CNS

4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a
waypoint selection submenu allowing selection of active flight plan, nearest, recent, or airway waypoints).
5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of
waypoints and press the ENT Key.

FLIGHT
MANAGEMENT

6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

7) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new
flight plan is now in the list.

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SYSTEM
OVERVIEW

Flight plans can be imported from an SD Card or exported to an SD Card from the Stored Flight Plan Page.
Importing a Flight Plan from an SD Card

FLIGHT
INSTRUMENTS

1) Insert the SD card containing the flight plan in the top card slot on the MFD.
2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.
5) Turn either FMS Knob to highlight an empty or existing flight plan.

EIS

6) Press the IMPORT Softkey; or press the MENU Key, select “Import Flight Plan”, and press the ENT Key.
If an empty slot is selected, a list of the available flight plans on the SD card will be displayed.

AUDIO PANEL
& CNS

Or:

If an existing flight plan is selected, an “Overwrite existing flight plan? OK or CANCEL” prompt is displayed.
Press the ENT Key to choose to overwrite the selected flight plan and see the list of available flight plans on the
SD card. If overwriting the existing flight plan is not desired, select “CANCEL” using the FMS Knob, press the
ENT Key, select another flight plan slot, and press the IMPORT Softkey again.

FLIGHT
MANAGEMENT

7) Turn the small FMS Knob to highlight the desired flight plan for importing.
8) Press the ENT Key to initiate the import.
9) Press the ENT Key again to confirm the import.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

List of Flight Plans to Import &
Details for the Selected File

APPENDICES

Import/Export Softkeys

Import Successful

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INDEX

Figure 5-57 Flight Plan Import

193

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Note: If the imported flight plan contains a waypoint with a name that duplicates the name of a waypoint

FLIGHT
INSTRUMENTS

already stored on the system, the system compares the coordinates of the imported waypoint with those of
the existing waypoint. If the coordinates are different, the imported waypoint is automatically renamed by
adding characters to the end of the name.
Exporting a Flight Plan to an SD Card
1) Insert the SD card into the top card slot on the MFD.
2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD.

EIS

3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.

AUDIO PANEL
& CNS

5) Turn the large FMS Knob to highlight the flight plan to be exported.
6) Press the EXPORT Softkey; or press the MENU Key, select “Export Flight Plan”.
7) If desired, change the name for the exported file by turning the large FMS Knob to the left to highlight the
name, then use the small and large FMS knobs to enter the new name, and press the ENT Key.

FLIGHT
MANAGEMENT

8) Press the ENT Key to initiate the export.

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

9) Press the ENT Key to confirm the export.

Import/Export Softkeys

Stored Flight Plan to be Exported &
Exported Flight Plan Name

Export Successful

INDEX

Figure 5-58 Flight Plan Export

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OVERVIEW

Adding Waypoints to an Existing Flight Plan

FLIGHT
INSTRUMENTS

Waypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the
desired point of insertion, enter the waypoint, and it is added in front of the selected waypoint. Flight plans
are limited to 99 waypoints (including waypoints within airways and procedures). If the number of waypoints
in the flight plan exceeds 99, the message “Flight plan is full. Remove unnecessary waypoints.” appears and the
new waypoint(s) are not added to the flight plan.

Stored Flight Plan Selected

EIS

- Memory Slot
- Comment
- Procedure Identifier
- Waypoint Identifier
- Airway Identifier
- Desired Track to Waypoint
- Distance to Waypoint
- Waypoint Altitude Constraint

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Softkeys
Figure 5-59 Stored Flight Plan Page

AFCS
ADDITIONAL
FEATURES

Flight Plan Full Message
APPENDICES

Figure 5-60 Active Flight Plan Page - FPL Full
INDEX

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OVERVIEW

Flight Management
Adding a waypoint to a stored flight plan:
1) On the Flight Plan Catalog Page, press the FMS Knob to activate the cursor.

FLIGHT
INSTRUMENTS

2) Highlight the desired flight plan.
3) Press the EDIT Softkey; or press the ENT Key, turn the large FMS Knob clockwise to select “EDIT” and press the
ENT Key. The Stored Flight Plan Page is displayed.
4) Select the point in the flight plan to add the new waypoint. The new waypoint is placed directly in front of the
highlighted waypoint.

EIS

5) Enter the identifier, facility, or city of the new waypoint.
6) Press the ENT Key. The new waypoint now exists in the flight plan.
Note: If the identifier entered in the Waypoint Information Window has duplicates, a Duplicate Waypoint

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Window is displayed. Use the FMS Knob to select the correct waypoint.

Figure 5-61 Duplicate Waypoints Window
ADDITIONAL
FEATURES

Adding a waypoint to the active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (not required on the PFD).

APPENDICES

3) Select the point in the flight plan before which to add the new waypoint. The new waypoint is placed directly
in front of the highlighted waypoint.
4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway
waypoints).

INDEX

5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of
waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered.

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Flight Management
SYSTEM
OVERVIEW

Creating and adding user waypoints to the active flight plan:
1) Press the Joystick to activate the panning function on the Active Flight Plan Page and pan to the map location
of the desired user waypoint.

FLIGHT
INSTRUMENTS

2) Press the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and press the ENT Key. The user
waypoint is created with a name of USRxxx (using the next available in sequence) and is added to the end of
the active flight plan.

Adding Airways to a Flight Plan

EIS

Airways can be added to the active flight plan or any stored flight plan. Choose a flight plan (add the desired
airway entry point if not already in the flight plan), select the waypoint after the desired airway entry point,
select the airway, and it is added in front of the selected waypoint. An airway can only be loaded if there is a
waypoint in the flight plan that is part of the desired airway and is not part of an arrival or approach procedure.
The G1000 also anticipates the desired airway and exit point based on loaded flight plan waypoints.

AUDIO PANEL
& CNS

Airway Entry Waypoint

FLIGHT
MANAGEMENT

Selected Airway
Airways Available at TOP
Airway Waypoint
Sequence

HAZARD
AVOIDANCE

Preview of
Selected Airway

AFCS
ADDITIONAL
FEATURES

Figure 5-62 Select Airway Page - Selecting Airway

Adding an airway to a flight plan:
1) Press the FPL Key.

APPENDICES

2) Press the FMS Knob to activate the cursor (not required on the PFD).
3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not
a valid airway entry point, a valid entry point should be entered at this time.

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INDEX

4) Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey, or press the MENU Key and
select “Load Airway”. The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu
item is available only when a valid airway entry waypoint has been chosen (the waypoint ahead of the cursor
position).

197

SYSTEM
OVERVIEW

Flight Management
5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are
shown first in the list, followed by “all” altitude airways, and then high altitude airways.

FLIGHT
INSTRUMENTS

6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is
highlighted.
7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted.

Airway Entry Waypoint
EIS

Selected Airway
Selected Exit Point

AUDIO PANEL
& CNS

Preview of
Selected Airway
Selected Airway Exit
Point

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Airway Exit Points
Available

ADDITIONAL
FEATURES

AFCS

Figure 5-63 Select Airway Page - Selecting Exit Point

Inserted Airway Header

INDEX

APPENDICES

- Airway Identifier: [airway
identifier].[exit waypoint identifier]
(e.g., V4.SLN)

Figure 5-64 Active Flight Plan Page - Airway Inserted

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SYSTEM
OVERVIEW

Restrictions on Adding Airways
Some airways have directional restrictions on all or part of the route. Airway “A2” in Europe has a directional
restriction over the whole route such that it can be flown only in the direction MTD-ABB-BNE-DEVAL.

FLIGHT
INSTRUMENTS

Airway “UR975” in North Africa has more complicated directional restrictions within the list of airway
waypoints AMANO, VAKOR, LIBRO NELDA, DIRKA, GZO, KOSET, and SARKI:
• Starting from AMANO, the airway can be flown only to LIBRO.
• Starting from SARKI, the airway can be flown only to LIBRO.
• Between NELDA and GZO, the airway can be flown in either direction.

EIS

In the US, airways that are “one-way” for specified hours of operation are not uncommon. These airways
are always bidirectional in the G1000 database.

AUDIO PANEL
& CNS

The system only allows correct airway sequences to be inserted. If the pilot subsequently inverts the flight
plan, the system inverts the airway waypoint sequence and removes the airway header.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Flight Management

Adding Procedures to a Stored Flight Plan

FLIGHT
INSTRUMENTS

The G1000 allows the pilot to insert pre-defined instrument procedures from the navigation database into a
flight plan. The procedures are designed to facilitate routing of traffic leaving an airport (departure), arriving at
an airport (arrival), and landing at an airport (approach). See the procedures section for more details.

EIS

Flight Plan Name

AUDIO PANEL
& CNS

Flight Plan Waypoint
List

FLIGHT
MANAGEMENT

Softkeys

Load Departure Load Arrival Load Approach Activate Flight Plan -

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Figure 5-65 Stored Flight Plan Page

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Flight Management
SYSTEM
OVERVIEW

Departure (DP)

FLIGHT
INSTRUMENTS

A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can
be loaded at a time in a flight plan. The route is defined by selection of a departure, the transition waypoints,
and a runway.

Departure Airport

EIS

Selected
Departure
Departures Available at
KMCI

AUDIO PANEL
& CNS

Preview of
Selected
Departure

Departure Waypoint
Sequence

FLIGHT
MANAGEMENT

Figure 5-66 Departure Loading Page - Selecting the Departure
HAZARD
AVOIDANCE

Loading a departure procedure into a stored flight plan:
1) Select a stored flight plan from the Flight Plan Catalog Page.

AFCS

2) Press the EDIT Softkey; or press the MENU Key, select ‘EDIT FLIGHT PLAN’, and press the ENT Key. The Stored
Flight Plan Page is displayed.
3) Press the LD DP Softkey; or press the MENU Key, select “Load Departure”, and press the ENT Key. The
Departure Loading Page is displayed.

ADDITIONAL
FEATURES

4) Select a departure. Press the ENT Key.
5) Select a transition for the selected departure. Press the ENT Key.
6) Select a runway served by the selected departure, if required. Press the ENT Key.

APPENDICES

7) Press the ENT Key to load the selected departure procedure.

INDEX

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OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

Departure Airport

Selected
Departure

Selected Runway

AUDIO PANEL
& CNS

EIS

Preview of
Selected
Departure
Selected
Departure End
Point

Selected Transition
Departure Transition Points
Available

FLIGHT
MANAGEMENT

Figure 5-67 Departure Loading Page - Selecting Transition

HAZARD
AVOIDANCE

Inserted Departure Header

APPENDICES

ADDITIONAL
FEATURES

AFCS

- Departure Identifier: [departure
airport]-[departure runway].
[departure transition].
[departure end point]
(e.g., KMKC-ALL.WLDCT2.SLN)

INDEX

Figure 5-68 Stored Flight Plan Page - Departure Inserted

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Flight Management
SYSTEM
OVERVIEW

Arrival (STAR)

FLIGHT
INSTRUMENTS

A Standard Terminal Arrival (STAR) is loaded at the destination airport in the flight plan. Only one arrival
can be loaded at a time in a flight plan. The route is defined by selection of an arrival, the transition waypoints,
and a runway.

Destination Airport

EIS

Selected Arrival

Arrivals Available at KCOS

AUDIO PANEL
& CNS

Selected Runway
Arrival Waypoint Sequence
Preview of
Selected Arrival

FLIGHT
MANAGEMENT

Figure 5-69 Arrival Loading Page - Selecting the Arrival
HAZARD
AVOIDANCE

Loading an arrival procedure into a stored flight plan:
1) Select a stored flight plan from the Flight Plan Catalog Page.

AFCS

2) Press the EDIT Softkey; or press the MENU Key, select ‘EDIT FLIGHT PLAN’, and press the ENT Key. The Stored
Flight Plan Page is displayed.
3) Press the LD STAR Softkey; or press the MENU Key, select “Load Arrival”, and press the ENT Key. The Arrival
Loading Page is displayed.

ADDITIONAL
FEATURES

4) Select an arrival. Press the ENT Key.
5) Select a transition for the selected arrival. Press the ENT Key.
6) Select a runway served by the selected arrival, if required. Press the ENT Key.

APPENDICES

7) Press the ENT Key to load the selected arrival procedure.

INDEX

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OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

Destination Airport
Selected Arrival
Selected Transition
Transitions Available with
DBRY1
Arrival Waypoint Sequence

AUDIO PANEL
& CNS

EIS

Preview of
Selected Arrival

FLIGHT
MANAGEMENT

Figure 5-70 Arrival Loading Page - Selecting the Transition

HAZARD
AVOIDANCE

Inserted Arrival Header

APPENDICES

ADDITIONAL
FEATURES

AFCS

- Arrival Identifier:
[arrival airport]-[arrival transition].
[arrival].[arrival runway]
(e.g., KCOS-TBE.DBRY1.ALL)

INDEX

Figure 5-71 Stored Flight Plan Page - Arrival Inserted

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Flight Management
SYSTEM
OVERVIEW

Approach (APPR)

FLIGHT
INSTRUMENTS

An Approach Procedure (APPR) can be loaded at any airport that has an approach available. Only one
approach can be loaded at a time in a flight plan. The route for a selected approach is defined by designating
transition waypoints.

Destination Airport

EIS

Selected
Approach

Approaches Available at
KCOS
AUDIO PANEL
& CNS

Barometric Minimum
Preview of
Selected
Approach

Approach Waypoint
Sequence

FLIGHT
MANAGEMENT

Figure 5-72 Approach Loading Page - Selecting the Approach
HAZARD
AVOIDANCE

Loading an approach procedure into a stored flight plan:
1) Select a stored flight plan from the Flight Plan Catalog Page.

AFCS

2) Press the EDIT Softkey; or press the MENU Key, select ‘EDIT FLIGHT PLAN’, and press the ENT Key. The Stored
Flight Plan Page is displayed.
3) Press the LD APR Softkey; or press the MENU Key, select “Load Approach”, and press the ENT Key. The
Approach Loading Page is displayed.

ADDITIONAL
FEATURES

4) Select an approach. Press the ENT Key.
5) Select a transition for the selected approach. Press the ENT Key.
6) Press the ENT Key to load the selected approval procedure.

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

Destination Airport

Selected
Approach

Selected Transition
Transitions Available with
Selected Approach

AUDIO PANEL
& CNS

EIS

Preview of
Selected
Approach

Barometric Minimum
Approach Waypoint
Sequence
Load Approach?

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Figure 5-73 Approach Loading Page - Selecting the Transition

Inserted Approach Header

ADDITIONAL
FEATURES

AFCS

- Approach Identifier: [approach
airport].[runway and approach type]
(e.g., KCOS-RNAV 35RGPS LPV)

INDEX

APPENDICES

Figure 5-74 Stored Flight Plan Page - Approach Inserted

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SYSTEM
OVERVIEW

Flight Plan Storage

FLIGHT
INSTRUMENTS

The G1000 can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when
the G1000 is powered off or when another flight plan is activated. Details about each stored flight plan can be
viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page.
Viewing information about a stored flight plan:
1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.

EIS

3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired flight plan.
4) The Flight Plan Information is displayed showing departure, destination, total distance, and enroute safe altitude
information for the selected Flight Plan.

AUDIO PANEL
& CNS

5) Press the EDIT Softkey to open the Stored Flight Plan Page and view the waypoints in the flight plan.
6) Press the FMS Knob to exit the Stored Flight Plan Page.

FLIGHT
MANAGEMENT

Flight Plan Name
(Comment)
Preview of Selected
Flight Plan

Selected Flight Plan

HAZARD
AVOIDANCE

Stored Flight Plan Info

AFCS

- Departure Airport
- Destination Airport
- Total Flight Plan Distance
- Enroute Safe Altitude

ADDITIONAL
FEATURES

Stored FPL Editing
Softkeys
Figure 5-75 Stored Flight Plan Information

Storing an active flight plan from the Active Flight Plan Page or the Active Flight Plan Window:
APPENDICES

1) Press the MENU Key.
2) Highlight ‘Store Flight Plan’.
3) Press the ENT Key.

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INDEX

4) With ‘OK’ highlighted, press the ENT Key. The flight plan is stored in the next available position in the flight
plan list on the Flight Plan Catalog Page.

207

SYSTEM
OVERVIEW

Flight Management
Sort Flight Plans

FLIGHT
INSTRUMENTS

The stored flight plans can be sorted alphanumerically based on the flight plan name (comment) assigned
to each flight plan.
Sorting by comment (flight plan name):
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the MENU Key.
3) Highlight ‘Sort By Comment’ and press the ENT Key. A confirmation window is displayed.

EIS

4 ) With ‘OK’ highlighted, press the ENT Key to change flight plan ordering. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.

AUDIO PANEL
& CNS

Activate a Flight Plan
Activating a stored flight plan erases the active flight plan and replaces it with the flight plan being activated.
Inverting a stored flight plan reverses the waypoint order and activates it.

FLIGHT
MANAGEMENT

1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.

HAZARD
AVOIDANCE

Activating a stored flight plan on the MFD:

4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.

2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
3) Press the ACTIVE Softkey; or press the MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The
‘Activate Stored Flight Plan?’ window is displayed.

Inverting and activating a stored flight plan on the MFD:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.

AFCS

2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
3) Press the INVERT Softkey; or press the MENU Key, highlight ‘Invert & activate FPL?’, and press the ENT Key.
The ‘Invert and activate stored flight plan?’ window is displayed.

ADDITIONAL
FEATURES

4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.

Copy a Flight Plan

APPENDICES

The G1000 allows copying a flight plan into a new flight plan memory slot, allowing editing, etc., without
affecting the original flight plan. This can be used to duplicate an existing stored flight plan for use in creating
a modified version of the original stored flight plan.
Copying a stored flight plan on the MFD:

INDEX

1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.

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Flight Management
SYSTEM
OVERVIEW

3) Press the COPY Softkey; or press the MENU Key, highlight ‘Copy Flight Plan’, and press the ENT Key. The ‘Copy
to Flight Plan XX?’ window is displayed.

FLIGHT
INSTRUMENTS

4) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel the request, press the CLR Key, or
highlight ‘CANCEL’ and press the ENT Key.

Delete a Stored Flight Plan
Individual or all stored flight plans can be deleted from the G1000 memory.
Deleting a stored flight plan:

EIS

1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.

AUDIO PANEL
& CNS

3) Press the DELETE Softkey; press the CLR Key; or press the MENU Key, highlight ‘Delete Flight Plan’, and press
the ENT Key. The ‘Delete Flight Plan XX?’ window is displayed.
4) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel the request, press the CLR Key, or
highlight ‘CANCEL’ and press the ENT Key.

FLIGHT
MANAGEMENT

Deleting all stored flight plans:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the MENU Key.
3) Highlight ‘Delete All’ and press the ENT Key. A ‘Delete all flight plans?’ confirmation window is displayed.

HAZARD
AVOIDANCE

4) With ‘OK’ highlighted, press the ENT Key to delete all flight plans. To cancel the request, press the CLR Key, or
highlight ‘CANCEL’ and press the ENT Key.

Flight Plan Editing

AFCS

The active flight plan or any stored flight plan can be edited. The edits made to the active flight plan affect
navigation as soon as they are entered.

Deleting the Active Flight Plan

ADDITIONAL
FEATURES

The G1000 allows deleting an active flight plan. Deleting the active flight plan suspends navigation by the
G1000.
Deleting the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).

APPENDICES

2) Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The ‘Delete all waypoints in flight
plan?’ window is displayed.
3) With ‘OK’ highlighted, press the ENT Key to delete the active flight plan. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.

INDEX

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SYSTEM
OVERVIEW

Flight Management
Deleting Flight Plan Items

FLIGHT
INSTRUMENTS

Individual waypoints, entire airways, and entire procedures can be deleted from a flight plan. Some waypoints
in the final approach segment (such as the FAF or MAP) can not be deleted individually. Attempting to delete
a waypoint that is not allowed results in a window displaying ‘Invalid flight plan modification.’
Deleting an individual waypoint from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).

EIS

2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the waypoint to be deleted.
3) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed.

AUDIO PANEL
& CNS

4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.

Deleting an entire airway from the active flight plan:

FLIGHT
MANAGEMENT

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the white header of the airway to be deleted.
3) Press the CLR Key. The ‘Remove ?’ window is displayed.

HAZARD
AVOIDANCE

4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.

Deleting an entire procedure from the active flight plan:
AFCS

ADDITIONAL
FEATURES

3) Press the CLR Key. The ‘Remove from flight plan?’ window is displayed.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.

APPENDICES

Or:

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove ’.
3) Press the ENT Key. The ‘Remove from flight plan?’ window is displayed.

INDEX

4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.

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SYSTEM
OVERVIEW

Deleting an individual waypoint from a stored flight plan:
1) Press the FPL Key to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.

FLIGHT
INSTRUMENTS

3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
5) Turn the large FMS Knob to highlight the waypoint to be deleted.

EIS

6) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.

AUDIO PANEL
& CNS

8) Press the FMS Knob to remove the flashing cursor.

Deleting an entire airway from a stored flight plan:
1) Press the FPL Key to display the Active Flight Plan Page.

FLIGHT
MANAGEMENT

2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.

HAZARD
AVOIDANCE

5) Turn the large FMS Knob to highlight the white header of the airway to be deleted.
6) Press the CLR Key. The ‘Remove ?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
8) Press the FMS Knob to remove the flashing cursor.

AFCS

Deleting an entire procedure from a stored flight plan:
1) Press the FPL Key to display the Active Flight Plan Page.

ADDITIONAL
FEATURES

APPENDICES

5) Turn the large FMS Knob to highlight the white header of the procedure to be deleted.
6) Press the CLR Key. The ‘Remove from flight plan?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.

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INDEX

8) Press the FMS Knob to remove the flashing cursor.

Or:

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

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SYSTEM
OVERVIEW

Flight Management
1) Press the FPL Key to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.

FLIGHT
INSTRUMENTS

3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
5) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove ’.
6) Press the ENT Key. The ‘Remove from flight plan?’ window is displayed.
EIS

7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
8) Press the FMS Knob to remove the flashing cursor.

AUDIO PANEL
& CNS

Changing Flight Plan Comments (Names)
The comment field (or name) of each flight plan can be changed to something that is useful for identification
and sorting.

FLIGHT
MANAGEMENT

Changing the active flight plan comment:
1) Press the FPL Key to display the Active Flight Plan Page.
2) Press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the comment field.
3) Use the FMS Knobs to edit the comment.

HAZARD
AVOIDANCE

4) Press the ENT Key to accept the changes.
5) Press the FMS Knob to remove the flashing cursor.

Changing a stored flight plan comment:

AFCS

1) Press the FPL Key to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
ADDITIONAL
FEATURES

4) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
5) Turn the large FMS Knob to highlight the comment field.
6) Use the FMS Knobs to edit the comment.

APPENDICES

7) Press the ENT Key to accept the changes.
8) Press the FMS Knob to remove the flashing cursor.

Along Track Offsets

INDEX

A waypoint having an “along track offset” distance from an existing waypoint can be entered into a flight plan.
Along track offset waypoints lie along the path of the existing flight plan, and can be used to make the system
reach a specified altitude before or after reaching the specified flight plan waypoint. Offset distances can be

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OVERVIEW

entered from 1 to 99 nm in increments of 1 nm. Entering a negative offset distance results in an along track
offset waypoint inserted before the selected waypoint, whereas entering a positive offset distance results in an
along track offset waypoint inserted after the selected waypoint. Multiple offset waypoints are allowed.

FLIGHT
INSTRUMENTS

A waypoint must be adjacent to its parent waypoint in the flight plan, so the system limits the along-track
distance to less than the length of the leg before or after the selected waypoint. If the selected waypoint is the
active waypoint, the distance is limited to less than the distance to go to the active waypoint. Assigning an along
track offset to a leg with indeterminate length is not permitted. An along track offset is not allowed at or after
the final approach fix of an approach.

EIS

An along track offset distance cannot be modified once entered. If the along track offset distance must be
changed, the existing along track offset waypoint must be deleted and a new one created with the new offset
distance.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Along Track Offset
Waypoint and Distance
from Flight Plan Waypoint
Along Track
Offset Waypoint
and Distance

HAZARD
AVOIDANCE
AFCS

Figure 5-76 Along Track Offset

ADDITIONAL
FEATURES

Entering an along track offset distance:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the waypoint for the along track offset.

APPENDICES

3) Press the ATK OFST Softkey (MFD only); or press the MENU Key, highlight ‘Create ATK Offset Waypoint’, and
press the ENT Key.
4) Enter a positive or negative offset distance in the range of +/- 1 to 99 nm (limited by leg distances).
5) Press the ENT Key to create the offset waypoint.

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6) Press the FMS Knob to remove the flashing cursor.

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Flight Management

Parallel Track

FLIGHT
INSTRUMENTS

The Parallel Track (PTK) feature allows creation of a parallel course offset of 1 to 50 nm left or right of the
current flight plan. When Parallel Track is activated, the course line drawn on the map pages shows the parallel
course, and waypoint names have a lower case “p” placed after the identifier.
Using direct-to, loading an approach, a holding pattern, or editing and activating the flight plan automatically
cancels Parallel Track. Parallel Track is also cancelled if a course change occurs greater than 120° or the parallel
tracks overlap as a result of the course change.

AUDIO PANEL
& CNS

EIS

Note: Vertical navigation is unavailable while the Parallel Track feature is active.

Selecting Parallel
Track

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Active Flight Plan prior to Parallel Track

Figure 5-77 Active Flight Plan Window - Selecting Parallel Track

AFCS

Activating parallel track:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)

ADDITIONAL
FEATURES

2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed
with the direction field highlighted.
3) Turn the small FMS Knob to select ‘Left’ or ‘Right’ and press the ENT Key. The ‘DISTANCE’ field is highlighted.

APPENDICES

4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘ACTIVATE PARALLEL
TRACK’ is highlighted.

INDEX

5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track
activation.

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Offset Direction
Offset Distance

FLIGHT
INSTRUMENTS

Activation Prompt

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-78 Parallel Track Window

HAZARD
AVOIDANCE

Parallel Track Waypoints
Parallel Track
Original Track

AFCS

- TIFTO-p
- TOP-p
- ULNAZ-p
- ...
- LAA-p
Activating Parallel Track
affects the entire active
flight segment (e.g.,
enroute)

ADDITIONAL
FEATURES
APPENDICES

Figure 5-79 Parallel Track Active

INDEX

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EIS

FLIGHT
INSTRUMENTS

If the parallel track proposed by the offset direction and distance is not allowed by the system, the activation
prompt is displayed, but disabled. Parallel Track cannot be activated if a course is set using direct-to or if the
active leg is the first leg of the departure procedure. Attempting to activate parallel track with these conditions
results in the message ‘Parallel Track Unavailable Invalid Route Geometry’. If an approach leg is active the status
indicates that the system is unable to activate the parallel track with the message ‘Parallel Track Unavailable
Approach Leg Active’. If the offset direction and distance results in an unreasonable route geometry the status
indicates that the system is unable to activate the parallel track because of invalid geometry.

Subdued Prompt
AUDIO PANEL
& CNS

(Unavailable)

Unavailable Status

Approach
Active

FLIGHT
MANAGEMENT

Invalid
Geometry

HAZARD
AVOIDANCE

Figure 5-80 Parallel Track Unavailable

AFCS

If the active leg is not a track between two fixes (TF) or a course to a fix (DF) leg, the status
indicates that the system is unable to activate the parallel track because parallel track is not available for the
active leg type.

Offset Direction &
Distance Subdued
(Unavailable)

ADDITIONAL
FEATURES

Cancel Prompt

APPENDICES

Active Status

INDEX

Figure 5-81 Cancelling Parallel Track

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Cancelling parallel track:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)

FLIGHT
INSTRUMENTS

2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed
with ‘CANCEL PARALLEL TRACK?’ highlighted.
3) Press the ENT Key.

Activating a Flight Plan Leg

EIS

The G1000 allows selection of a highlighted leg as the “active leg” (the flight plan leg which is currently
used for navigation guidance).
Activating a flight plan leg:

AUDIO PANEL
& CNS

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the destination waypoint for the desired leg.

FLIGHT
MANAGEMENT

3) Press the ACT LEG Softkey (MFD only); or press the MENU Key, highlight ‘Activate Leg’, and press the ENT Key.
A confirmation window is displayed with ‘ACTIVATE’ highlighted.
4) Press the ENT Key to activate the flight plan leg. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press
the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.

HAZARD
AVOIDANCE
AFCS

Current
Active Leg

Selected Destination
Waypoint

ADDITIONAL
FEATURES
APPENDICES

Activate Leg Softkey
Figure 5-82 Active Flight Plan Page - Selecting the Leg Destination Waypoint

INDEX

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FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Flight Management

EIS

New Active
Flight Plan Leg

AUDIO PANEL
& CNS

Confirmation Window
Figure 5-83 Active Flight Plan Page - New Active Leg

FLIGHT
MANAGEMENT

Inverting a Flight Plan
Any flight plan may be inverted (reversed) for navigation back to the original departure point.
Inverting the active flight plan:

HAZARD
AVOIDANCE

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the MENU Key, highlight ‘Invert Flight Plan’, and press the ENT Key. An ‘Invert Active Flight Plan?’
confirmation window is displayed.
3) Select ‘OK’.

AFCS

4) Press the ENT Key to invert and activate the active flight plan. To cancel, press the CLR Key, or highlight
‘CANCEL’ and press the ENT Key.

Inverting and activating a stored flight plan:
ADDITIONAL
FEATURES

1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be inverted.

APPENDICES

4) Press the INVERT Softkey; or press the MENU Key, select ‘Invert & Activate Flight Plan’ and press the ENT Key.
An ‘Invert and activate stored flight plan?’ confirmation window is displayed.
5) Select ‘OK’.

INDEX

6) Press the ENT Key to invert and activate the stored flight plan. To cancel, press the CLR Key, or highlight
‘CANCEL’ and press the ENT Key.

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Flight Plan Views

FLIGHT
INSTRUMENTS

Information about flight plans can be viewed in more than one way. The active flight plan can be configured
to show cumulative distance over the length of the flight plan or the distance for each leg of the flight plan;
and the active flight plan can be viewed in a narrow or wide view. In the wide view, additional information is
displayed: Fuel Remaining (FUEL REM), Estimated Time Enroute (ETE), Estimated Time of Arrival (ETA), and
Bearing to the waypoint (BRG).
Switching between leg-to-leg waypoint distance and cumulative waypoint distance:
1) Press the FPL Key on the MFD to display the Active Flight Plan Page.

EIS

2) Press the VIEW Softkey to display the CUM and LEG-LEG Softkeys.
3) Press the CUM Softkey to view cumulative waypoint distance, or press the LEG-LEG Softkey to view leg-to-leg
waypoint distance.

AUDIO PANEL
& CNS

4) Press the BACK Softkey to return to the top level active flight plan softkeys.
Active Flight Plan Leg to Leg Distance

Active Flight Plan Cumulative Distance

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey
Figure 5-84 Active Flight Plan - Leg to Leg vs. Cumulative Distance

Switching between wide and narrow view:
APPENDICES

1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
2) Press the VIEW Softkey to display the WIDE and NARROW Softkeys.
3) Press the WIDE Softkey to display the wide view, or press the NARROW Softkey to display the narrow view.

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4) Press the BACK Softkey to return to the top level active flight plan softkeys.

219

SYSTEM
OVERVIEW

Flight Management
Active Flight Plan Wide View

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Active Flight Plan Narrow View

WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey

FLIGHT
MANAGEMENT

Figure 5-85 Active Flight Plan - Wide vs. Narrow View

Collapsing Airways

HAZARD
AVOIDANCE

The G1000 allows airways on the active flight plan to be collapsed or expanded from the Active Flight Plan
Page/Window. When airways have been collapsed, it is indicated on the airway heading.
When airways are collapsed, leg-to-leg computed values such as DIS or ETE shown for the exit waypoint
reflects the total of all the legs on the airway that have been hidden in the collapsed display. The DTK value is
inhibited because it is not usable in this context.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

The Active Flight Plan Page always keeps the following three waypoints visible: “From” waypoint, “To”
waypoint, and the “Next” waypoint. To prevent one or more of these waypoints from being hidden in a collapsed
airway segment, the airway segment that contains either the “To” or the “Next” waypoint is automatically
expanded. When an airway is loaded, airways are automatically expanded to facilitate flight plan review.

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Q3.FEPOT Airway

FLIGHT
INSTRUMENTS

Collapsed View
Expanded View

EIS

Figure 5-86 Expanded/Collapsed Airways
AUDIO PANEL
& CNS

Collapsing/expanding the airways in the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)

FLIGHT
MANAGEMENT

2) Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and press the ENT Key. The airways are
collapsed/expanded.

Closest Point of FPL

HAZARD
AVOIDANCE

‘Closest Point of FPL’ calculates the bearing and closest distance at which a flight plan passes a reference
waypoint, and creates a new user waypoint along the flight plan at the location closest to a chosen reference
waypoint.
Determining the closest point along the active flight plan to a selected waypoint:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)

AFCS

2) Press the MENU Key, highlight ‘Closest Point of FPL’’, and press the ENT Key. A window appears with the
reference waypoint field highlighted.

ADDITIONAL
FEATURES

3) Enter the identifier of the reference waypoint and press the ENT Key. The G1000 displays the bearing (BRG) and
distance (DIS) to the closest point along the flight plan to the selected reference waypoint and creates a user
waypoint at this location. The name for the new user waypoint is derived from the identifier of the reference
waypoint.

APPENDICES
INDEX

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5.7 Vertical Navigation

FLIGHT
INSTRUMENTS

Note: The G1000 supports vertical navigation for all lateral leg types except for CA, CI, FA, FM, HA, HM, PI,

VA, VD, VI, VR, and VM. Vertical constraints are not retained in stored flight plans.

EIS

The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute
and teminal phases of flight. Guidance based on specified altitudes at waypoints in the active flight plan or to a
direct-to waypoint is provided. It includes vertical path guidance to a descending path, which is provided as a
linear deviation from the desired path. The desired path is defined by a line joining two waypoints with specified
altitudes or as a vertical angle from a specified waypoint/altitude. The vertical waypoints are integrated into the
active flight plan. Both manual and autopilot-coupled guidance are supported.
Current Vertical Navigation Profile

Current Vertical Navigation Profile
Enabled (valid data)

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Disabled (fields dashed)

ENBL VNV Softkey

CNCL VNV Softkey

ADDITIONAL
FEATURES

Figure 5-87 Enabling/Disabling Vertical Navigation

Enabling VNV guidance:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.

APPENDICES

2) Press the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable VNV’, and press the ENT Key. Vertical
navigation is enabled, and vertical guidance begins with the waypoint shown in the CURRENT VNV PROFILE box
(defaults first waypoint in the active flight plan with an altitude enabled for vertical navigation (e.g., HABUK)).

Disabling VNV guidance:

INDEX

1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical
navigation is disabled.

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OVERVIEW
FLIGHT
INSTRUMENTS

Canceling vertical navigation results in vertical deviation (V DEV), vertical speed required (VS REQ), and time
to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid. The Vertical Deviation Indicator (VDI)
and Required Vertical Speed Indicator (RVSI) on the PFD are removed, and the V DEV, VS REQ, and TIME TO
TOD items displayed in the CURRENT VNV PROFILE box are dashed. VNV remains disabled until manually
enabled. Vertical guidance in reversionary mode can only be enabled for a direct-to waypoint.

AUDIO PANEL
& CNS

Current Vertical Navigation Profile

EIS

The G1000 allows a vertical navigation direct-to to any waypoint in the active flight plan with an altitude
constraint “designated” for vertical guidance. Selecting the VNV Direct-to Softkey on the Active Flight Plan Page
allows the flight plan to be flown, while vertical guidance based on the altitude constraint at the VNV direct-to
waypoint is provided. The altitude change begins immediately and is spread along the flight plan from current
position to the vertical direct-to waypoint, not just along the leg for the direct-to waypoint. A direct-to with
altitude constraint activated by pressing the Direct-to Key also provides vertical guidance, but would bypass
flight plan waypoints between the current position in the flight plan and the direct-to waypoint. A top of descent
(TOD) point is computed based on the default flight path angle; descent begins once the TOD is reached.
Current Vertical Navigation Profile

Prior to VNV Direct-to

After VNV Direct-to

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

VNV Direct-To Softkey

VNV PROF Softkey
ADDITIONAL
FEATURES

Figure 5-88 Vertical Navigation Direct-To

Activating a vertical navigation direct-to:

APPENDICES

1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint.
Note: The selected waypoint must have a designated altitude constraint (light blue number) to be used. If

not, the first waypoint in the flight plan with a designated altitude constraint is selected.
INDEX

3) Select the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV Direct-To’, and press the ENT Key.
An ‘Activate vertical Direct-to to: NNNNNFT at XXXXXX?’ confirmation window is displayed.

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4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint.
5) Press the FMS Knob to remove the flashing cursor.

FLIGHT
INSTRUMENTS

The vertical navigation profile can be modified by directly entering a vertical speed target (VS TGT) and/or flight
path angle (FPA) in the CURRENT VNV PROFILE box.
Modifying the VS TGT and FPA:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.

EIS

2) Press the VNV PROF Softkey; or press the MENU Key, highlight ‘Select VNV Profile Window’, and press the ENT
Key. The cursor is now located in the CURRENT VNV PROFILE box.
3) Turn the FMS Knobs as needed to edit the values.

AUDIO PANEL
& CNS

4) Press the FMS Knob to remove the flashing cursor.

Altitude Constraints

FLIGHT
MANAGEMENT

The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical
navigation. These altitudes are, depending on the specific instance, manually entered or retrieved from the
published altitudes in the navigation database. The navigation database only contains altitudes for procedures
that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” then the altitude is not in the
database. In this case the altitude may be entered manually.
Displayed Text
Examples

HAZARD
AVOIDANCE

Cross AT
or ABOVE
5,000 ft

Large White Text
Large Light Blue Text

Cross AT
2,300 ft
AFCS

Small Light Blue Text
Cross AT
or BELOW
3,000 ft

Small Light Blue
Subdued Text

ADDITIONAL
FEATURES

Altitude Constraint
Examples

Small White Text with
Altitude Restriction Bar

INDEX

APPENDICES

Figure 5-89 Waypoint Altitude Constraints

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Light Blue Text

Light Blue Subdued Text
The system cannot use this
altitude in determining vertical
speed and deviation guidance
because of an invalid constraint
condition

Small
Text

Altitude is designated for use in giving
vertical speed and deviation guidance.
Altitude has been retrieved from the
navigation database or has been entered
manually and matches a published
altitude in the navigation database.

The system cannot use this
altitude in determining vertical
speed and deviation guidance
because of an invalid constraint
condition

EIS

Altitude has been entered manually.
Altitude is designated for use in giving
vertical speed and deviation guidance.
Altitude does not match the published
altitude in navigation database or no
published altitude exists.

FLIGHT
INSTRUMENTS

Large Altitude calculated by the system
Text estimating the altitude of the aircraft as
it passes over the navigation point. This
altitude is provided as a reference and is
not designated to be used in determining
vertical speed and deviation guidance.
Altitude is not designated to be used in
determining vertical speed and deviation
guidance. Altitude has been retrieved
from the navigation database and is
provided as a reference.

SYSTEM
OVERVIEW

White Text

AUDIO PANEL
& CNS

Table 5-8 Altitude Constraint Size and Color Coding

FLIGHT
MANAGEMENT

Altitudes associated with approach procedures are “auto-designated”. This means the system automatically
uses the altitudes loaded with the approach for giving vertical speed and deviation guidance. Note that these
altitudes are displayed as blue text up to, but not including the FAF. The FAF is always a “reference only”
altitude and cannot be designated, unless the selected approach does not provide vertical guidance. In this case,
the FAF altitude can be designated.

HAZARD
AVOIDANCE

Altitudes that have been designated for use in vertical guidance can be “un-designated” using the CLR Key.
The altitude is now displayed only as a reference. It is not used to give vertical guidance. Other displayed
altitudes may change due to re-calculations or be rendered invalid as a result of manually changing an altitude
to a non-designated altitude.
Designating a waypoint altitude to be used for vertical guidance:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.

AFCS

2) Press the FMS Knob, and turn to highlight the desired waypoint altitude.
3) Turn the small FMS Knob to enter editing mode.
4) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance.

ADDITIONAL
FEATURES

Designating a procedure waypoint altitude to be used for vertical guidance:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude.

APPENDICES

3) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance.

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INDEX

Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the nearest hundred. An
altitude constraint in feet above ground level (AGL) format is supported for airports. When a database altitude
restriction is displayed, the G1000 allows entry of a different altitude when creating a waypoint, effectively
overriding the database restriction (only before the FAF). When a database altitude restriction of type “AT or
ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the restriction to define the vertical
profile.

225

SYSTEM
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Flight Management
An altitude constraint is invalid if:
• Meeting the constraint requires the aircraft to climb

FLIGHT
INSTRUMENTS

• Meeting the constraint requires the maximum flight path angle (6° down) or maximum vertical speed (-6000
fpm) to be exceeded
• The altitude constraint results in a TOD behind the aircraft present position
• The constraint is within a leg type for which altitude constraints are not supported

EIS

• The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS
WAAS approach)
• The altitude constraint is added to a waypoint past the FAF.
Entering/modifiying an altitude constraint:
AUDIO PANEL
& CNS

1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.

FLIGHT
MANAGEMENT

3) Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a flight level, turn the small
FMS Knob counter-clockwise past zero or clockwise past 9 on the first character, and the system automatically
changes to show units of Flight Level. Turn the large FMS Knob clockwise to highlight the first zero and enter
the three digit flight level.
4) Press the ENT Key to accept the altitude constraint; if the selected waypoint is an airport, an additional choice
is displayed. Turn the small FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude.

HAZARD
AVOIDANCE

Altitude constraints can be modified or deleted after having been added to the flight plan. In the event
an altitude constraint is deleted and the navigation database contains an altitude restriction for the lateral
waypoint, the G1000 displays the altitude restriction from the database provided no predicted altitude
can be provided. The G1000 also provides a way to reinstate a published altitude constraint that has been
edited.

AFCS

Deleting an altitude constraint provided by the navigation database:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.

ADDITIONAL
FEATURES

2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
3) Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation window is displayed.
4) Select ‘OK’ and press the ENT Key.

Deleting an altitude constraint that has been manually entered:

APPENDICES

1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is
displayed.

INDEX

4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system
calculated altitude, if available).

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SYSTEM
OVERVIEW

Reverting a manually entered altitude constraint back to the navigation database value:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.

FLIGHT
INSTRUMENTS

3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is
displayed.
4) Select ‘REVERT’ and press the ENT Key. The altitude is changed to the navigation database value.
5) Press the FMS Knob to remove the flashing cursor.

EIS

Modifying a system calculated altitude constraint:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.

AUDIO PANEL
& CNS

3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ confirmation window is
displayed.
4) Select ‘EDIT’ and press the ENT Key.

FLIGHT
MANAGEMENT

5) Edit the value using the FMS Knobs, and press the ENT Key.
6) Press the FMS Knob to remove the flashing cursor.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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5.8 Procedures

FLIGHT
INSTRUMENTS

The G1000 can access the whole range of instrument procedures available. Departures (DPs), arrivals (STARs),
and non-precision and precision approaches (APPRs) are stored within the database and can be loaded using the
Procedures (PROC) Key.

AUDIO PANEL
& CNS

EIS

The selected procedure for the departure or arrival airport is added to the active flight plan. No waypoints are
required to be in the active flight plan to load procedures; however, if the departure and arrival airport are already
loaded, the procedure loading window defaults to the appropriate airport, saving some time selecting the correct
airport on the Procedure Loading Page. Whenever an approach is selected, the choice to either “load” or “activate”
is given. “Loading” adds the approach to the end of the flight plan without immediately using it for navigation
guidance. This allows continued navigation via the intermediate waypoints in the original flight plan, but keeps
the procedure available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds
the procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in
the approach.

Departures

FLIGHT
MANAGEMENT

A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be
loaded at a time in a flight plan. If a departure is loaded when another departure is already in the active flight
plan, the new departure replaces the previous departure. The route is defined by selection of a departure, the
transition waypoints, and a runway.

HAZARD
AVOIDANCE

Loading a Departure into the Active Flight Plan
Loading a departure into the active flight plan using the PROC Key:
1) Press the PROC Key. The Procedures Window is displayed.
2) Highlight ‘SELECT DEPARTURE’.

AFCS

3) Press the ENT Key. The Departure Loading Page is displayed.
4) Select a departure from the list and press the ENT Key.
5) Select a runway (if required) and press the ENT Key.
ADDITIONAL
FEATURES

6) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted.

INDEX

APPENDICES

7) Press the ENT Key to load the departure procedure.

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SYSTEM
OVERVIEW

Available Procedure Actions

Departure Airport

FLIGHT
INSTRUMENTS
EIS

Departure Preview

AUDIO PANEL
& CNS

Loaded Procedures

Departure Choices

Selected Departure

FLIGHT
MANAGEMENT

Figure 5-90 Departure Selection
Loaded Departure

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Procedure Loading Page Selection Softkeys
Figure 5-91 Departure Loading

INDEX

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SYSTEM
OVERVIEW

Viewing available departures at an airport:

FLIGHT
INSTRUMENTS

Flight Management

2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and
press the ENT Key.

1) From the Airport Information Page (first page in the WPT group), press the DP Softkey. The Departure Information
Page is displayed, defaulting to the airport displayed on the Airport information Page.

3) Press the FMS Knob, then turn the large FMS Knob to highlight the Departure. The departure is previewed on
the map.

EIS

4) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor
moves to the Runway box. The departure is previewed on the map.
5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor
moves to the Transition box. The departure is previewed on the map.

AUDIO PANEL
& CNS

6) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor
moves to the Sequence box. The departure is previewed on the map.
7) Press the INFO Softkey to return to the Airport Information Page.

FLIGHT
MANAGEMENT

Removing a Departure from the Active Flight Plan
When plans change while flying IFR, departures can be easily removed from the Active Flight Plan.
Removing a departure procedure from the active flight plan:

HAZARD
AVOIDANCE

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the MENU Key, and highlight ‘Remove Departure’.
3) Press the ENT Key. A confirmation window is displayed listing the departure procedure.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.

AFCS

Or:

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)

ADDITIONAL
FEATURES

2) Press the FMS Knob, and turn to highlight the departure header in the active flight plan.
3) Press the CLR Key. A confirmation window is displayed listing the departure procedure.

INDEX

APPENDICES

4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.

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OVERVIEW

Arrivals

FLIGHT
INSTRUMENTS

A Standard Terminal Arrival (STAR) can be loaded at any airport that has one available. Only one arrival
can be loaded at a time in a flight plan. If an arrival is loaded when another arrival is already in the active
flight plan, the new arrival replaces the previous arrival. The route is defined by selection of an arrival, the
transition waypoints, and a runway.

Loading an Arrival into the Active Flight Plan
Loading an arrival into the active flight plan using the PROC Key:

EIS

1) Press the PROC Key. The Procedures Window is displayed.
2) Highlight ‘SELECT ARRIVAL’.
3) Press the ENT Key. The Arrival Loading Page is displayed.

AUDIO PANEL
& CNS

4) Select an arrival from the list and press the ENT Key.
6) Select a transition (if required) and press the ENT Key.
7) Select a runway (if required) and press the ENT Key. ‘LOAD?’ is highlighted.

Available Procedure Actions

FLIGHT
MANAGEMENT

8) Press the ENT Key to load the arrival procedure.
Destination Airport

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Loaded Procedures

Arrival Preview

Arrival Choices
APPENDICES

Figure 5-92 Arrival Selection

INDEX

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SYSTEM
OVERVIEW

Flight Management
Loaded Arrival

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Selected Arrival

Procedure Loading Page Selection Softkeys

FLIGHT
MANAGEMENT

Figure 5-93 Arrival Loading

Viewing available arrivals at an airport:

HAZARD
AVOIDANCE

1) From the Airport Information Page (first page in the WPT group), press the STAR Softkey. The Arrival Information
Page is displayed, defaulting to the airport displayed on the Airport Information Page.
2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and
press the ENT Key.
3) Press the FMS Knob, then turn the large FMS Knob to highlight the Arrival. The arrival is previewed on the
map.

AFCS

4) Turn the small FMS Knob to view the available arrivals. Press the ENT Key to select the arrival. The cursor moves
to the Transition box. The arrival is previewed on the map.

ADDITIONAL
FEATURES

5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor
moves to the Runway box. The arrival is previewed on the map.
6) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor
moves to the Sequence box. The arrival is previewed on the map.

INDEX

APPENDICES

7) Press the INFO Softkey to return to the Airport Information Page.

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SYSTEM
OVERVIEW

Removing an Arrival from the Active Flight Plan
When plans change while flying IFR, arrivals can be easily removed from the Active Flight Plan.

FLIGHT
INSTRUMENTS

Removing an arrival from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the MENU Key, and highlight ‘Remove Arrival’.
3) Press the ENT Key. A confirmation window is displayed listing the arrival procedure.

EIS

4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.
Or:

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
AUDIO PANEL
& CNS

2) Press the FMS Knob, and turn to highlight the arrival header in the active flight plan.
3) Press the CLR Key. A confirmation window is displayed listing the arrival procedure.

FLIGHT
MANAGEMENT

4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.

Approaches
NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some published approach procedures

HAZARD
AVOIDANCE

for the desired airport may not be displayed in the list of available approaches.

AFCS

An Approach Procedure (APPR) can be loaded at any airport that has one available, and provides guidance
for non-precision and precision approaches to airports with published instrument approach procedures.
Only one approach can be loaded at a time in a flight plan. If an approach is loaded when another approach
is already in the active flight plan, the new approach replaces the previous approach. The route is defined by
selection of an approach and the transition waypoints.

ADDITIONAL
FEATURES

Whenever an approach is selected, the choice to either “load” or “activate” is given. “Loading” adds the
approach to the end of the flight plan without immediately using it for navigation guidance. This allows
continued navigation via the intermediate waypoints in the original flight plan, but keeps the procedure
available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds the
procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in
the approach.

APPENDICES

When selecting an approach, a “GPS” designation to the right of the procedure name indicates the procedure
can be flown using the GPS receiver. Some procedures do not have this designation, meaning the GPS
receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for
primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or
ILS). The final course segment of ILS approaches, for example, must be flown by tuning the NAV receiver to
the proper frequency and selecting that NAV receiver on the CDI.

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INDEX

The G1000 WAAS GPS allows for flying LNAV, LNAV/VNAV, and LPV approaches according to the published
chart. LNAV+V is a standard LNAV approach with advisory vertical guidance provided for assistance in

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OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

maintaining a constant vertical glidepath similar to an ILS glideslope on approach. This guidance is displayed
on the G1000 PFD in the same location as the ILS glideslope using a magenta diamond. In all cases where
LNAV+V is indicated by the system during an approach, LNAV minima are used. The active approach type
is annunciated on the HSI as shown in the following table:

EIS

HSI Annunciation
Description
LNAV
GPS approach using published LNAV minima
LNAV+V
GPS approach using published LNAV minima.
Advisory vertical guidance is provided
L/VNAV
GPS approach using published LNAV/VNAV
minima
LPV
GPS approach using published LPV minima

Example on HSI

Approach Type
- LNAV
- LNAV+V
- L/VNAV
- LPV

AUDIO PANEL
& CNS

Table 5-9 Approach Types

Loading an Approach into the Active Flight Plan
Loading an approach into the active flight plan using the PROC Key:

FLIGHT
MANAGEMENT

1) Press the PROC Key. The Procedures Window is displayed.
2) Highlight ‘SELECT APPROACH’, and press the ENT Key. The Approach Loading Page is displayed.
3) Select an approach from the list and press the ENT Key.

HAZARD
AVOIDANCE

4) Select a transition (if required) and press the ENT Key.
5) Barometric Minimums
a) To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, and press the ENT Key. Turn the small FMS
Knob to select the altitude, and press the ENT Key.
Or:
AFCS

b) To skip setting minimums, press the ENT Key.

ADDITIONAL
FEATURES

6) Press the ENT Key with ‘LOAD?’ highlighted to load the arrival procedure; or turn the large FMS Knob to
highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure.
NOTE: When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED

INDEX

APPENDICES

FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV
receiver to fly the final course of the approach.

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SYSTEM
OVERVIEW

Available Procedure Actions

Destination Airport

FLIGHT
INSTRUMENTS
EIS

Approach Preview

AUDIO PANEL
& CNS

Loaded Procedures

Approach Choices

Selected Approach

FLIGHT
MANAGEMENT

Figure 5-94 Approach Selection
Loaded Approach

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Procedure Loading Page Selection Softkeys

LOAD or ACTIVATE? Annunciation
APPENDICES

Figure 5-95 Approach Loading

INDEX

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SYSTEM
OVERVIEW

Viewing available approaches at an airport:

FLIGHT
INSTRUMENTS

Flight Management

2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and
press the ENT Key.

1) From the Airport Information Page (first page in the WPT group), press the APR Softkey. The Departure
Information Page is displayed, defaulting to the airport displayed on the Airport information Page.

3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on
the map.

EIS

4) Turn the small FMS Knob to view the available approaches. Press the ENT Key to select the approach. The
cursor moves to the Runway box. The approach is previewed on the map.
5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor
moves to the Transition box. The approach is previewed on the map.

AUDIO PANEL
& CNS

6) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor
moves to the Sequence box. The approach is previewed on the map.
7) Press the INFO Softkey to return to the Airport Information Page.

FLIGHT
MANAGEMENT

Loading an approach into the active flight plan from the Nearest Airport Page:
1) Select the Nearest Airports Page.
2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired nearest airport. The airport is
previewed on the map.

HAZARD
AVOIDANCE

3) Press the APR Softkey; or press the MENU Key, highlight ‘Select Approach Window’, and press the ENT Key.
4) Turn the FMS Knob to highlight the desired approach.
5) Press the LD APR Softkey; or press the MENU Key, highlight ‘Load Approach’, and press the ENT Key. The
Approach Loading Page is displayed with the transitions field highlighted.

AFCS

6) Turn the FMS Knob to highlight the desired transition.
7) Barometric Minimums

ADDITIONAL
FEATURES

a) To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, and press the ENT Key. Turn the small FMS
Knob to select the altitude, and press the ENT Key. The ‘LOAD?’ field is highlighted.
Or:
b) To skip setting minimums, press the ENT Key. The ‘LOAD?’ field is highlighted.

INDEX

APPENDICES

8) Press the ENT Key with ‘LOAD?’ highlighted to load the arrival procedure; or turn the large FMS Knob to
highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. The G1000 continues
navigating the current flight plan until the approach is activated. When GPS is not approved for the selected
final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the
approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach.

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SYSTEM
OVERVIEW

Activating an Approach
A previously loaded approach can be activated from the Procedures Window.

FLIGHT
INSTRUMENTS

Activating a previously loaded approach:
1) Press the PROC Key. The Procedures Window is displayed with ‘Activate Approach’ highlighted.
2) Press the ENT Key to activate the approach.

EIS

In many cases, it may be easiest to “load” the full approach while still some distance away, enroute to the
destination airport. Later, if vectored to final, use the steps above to select ‘Activate Vector-To-Final’ — which
makes the inbound course to the FAF waypoint active.
Activating a previously loaded approach with vectors to final:
1) Press the PROC Key to display the Procedures Window.

AUDIO PANEL
& CNS

2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’ and press the ENT Key.

Loading and activating an approach using the MENU Key:

FLIGHT
MANAGEMENT

1) From the Approach Loading Page, press the MENU Key. The page menu is displayed with ‘Load & Activate
Approach’ highlighted.
2) Press the ENT Key. When GPS is not approved for the selected final approach course, the message ‘NOT
APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to
a NAV receiver to fly the final course of the approach.

HAZARD
AVOIDANCE

Removing an Approach from the Active Flight Plan
When plans change while flying IFR, approaches can be easily removed from the Active Flight Plan.
Removing an approach from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)

AFCS

2) Press the MENU Key, and highlight ‘Remove Approach’.
3) Press the ENT Key. A confirmation window is displayed listing the approach procedure.

ADDITIONAL
FEATURES

4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key.
Or:

1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the FMS Knob, and turn to highlight the approach header in the active flight plan.

APPENDICES

3) Press the CLR Key. A confirmation window is displayed listing the approach procedure.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.

INDEX

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OVERVIEW

Flight Management
Missed Approach
Activating a missed approach in the active flight plan:

FLIGHT
INSTRUMENTS

1) Press the PROC Key.
2) Turn the FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3) Press the ENT Key. The aircraft automatically sequences to the MAHP.

Or:

EIS

Press the Go-Around Button.

Course To Altitude

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is
not part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along
the runway centerline until the altitude required to safely make the first turn toward the MAHP is exceeded.
This altitude is provided by Jeppesen, and may be below, equal to, or above the published minimums for
this approach. In this case, if the aircraft altitude is below the specified altitude (6,368 feet) after crossing
the MAP, a direct-to is established to provide a course on runway heading until an altitude of 6,368 feet is
reached. After reaching 6,368 feet, a direct-to is established to the published MAHP (in this case MOGAL).
If the aircraft altitude is above the specified altitude after crossing the MAP, a direct-to is established to the
published fix (MOGAL) to begin the missed approach procedure.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

In some missed approach procedures this Course to Altitude leg may be part of the published procedure.
For example, a procedure may dictate a climb to 5,500 feet, then turn left and proceed to the Missed Approach
Hold Point (MAHP). In this case, the altitude would appear in the list of waypoints as ‘5500ft’. Again, if the
aircraft altitude is lower than the prescribed altitude, a direct-to is established on a Course to Altitude leg
when the missed approach procedure is activated.

APPENDICES

Course to Altitude Leg

INDEX

Figure 5-96 Course to Altitude

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SYSTEM
OVERVIEW

5.9 Trip Planning

FLIGHT
INSTRUMENTS

The G1000 allows the pilot to view trip planning information, fuel information, and other information for
a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. Weight
planning is also available, based on manually entered fuel data and the active flight plan (to estimate remaining
fuel).

Trip Planning

EIS

All of the input of data needed for calculation and viewing of the statistics is done on the Trip Planning Page
located in the AUX Page Group.
Selected Flight Plan Segment

- FPL Number/Cumulative Legs (CUM or REM) or Leg Number (NN)
- Waypoints Defining Selected Flight Plan/Flight Plan Leg
AUDIO PANEL
& CNS

Trip Planning Page Mode
- Automatic/Manual

FLIGHT
MANAGEMENT

Preview of Selected
Flight Plan/
Flight Plan Leg

Trip Input Data (sensor/pilot)

Trip Statistics

Desired Track Distance Est. Time Enroute Est. Time of Arrival Enroute Safe Altitude Sunrise Time (local) Sunset Time (local) -

HAZARD
AVOIDANCE

- Departure Time (local)
- Ground Speed
- Fuel Flow
- Fuel On Board Aircraft
- Calibrated Airspeed
- Indicated Altitude
- Barometric Pressure
- Total Air Temperature

Other Statistics

- Density Altitude
- True Airspeed (TAS)
AFCS

Fuel Statistics

Efficiency Total Endurance Remaining Fuel Remaining Endurance Fuel Required Total Range -

Softkeys

ADDITIONAL
FEATURES

- Automatic/Manual Page Mode
- Flight Plan/Waypoint Mode

Figure 5-97 Trip Planning Page

APPENDICES

The trip planning inputs are based on sensor inputs (automatic page mode) or on pilot inputs (manual page
mode). Some additional explanation of the sources for some of the inputs is as follows:
• Departure time (DEP TIME) - This defaults to the current time in automatic page mode. The computations
are from the aircraft present position, so the aircraft is always just departing.
• Calibrated airspeed (CALIBRATED AS) - The primary source is from the air data system, and the secondary
source of information is GPS ground speed.

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INDEX

• Indicated altitude (IND ALTITUDE) - The primary source is the barometric altitude, and the secondary source
of information is GPS altitude.

239

SYSTEM
OVERVIEW

Trip Statistics

FLIGHT
INSTRUMENTS

Flight Management

In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected,
the waypoints are the starting and ending waypoints of the selected flight plan.

The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning
inputs.

In flight plan mode (FPL) with a stored flight plan selected (NN), and a specific leg (NN) selected, the
waypoints are the endpoints of the selected leg.

EIS

In flight plan mode (FPL) with the active flight plan selected (00), and the remaining flight plan (REM)
selected, the ‘from’ waypoint is the present position of the aircraft and the ‘to’ waypoint is the endpoint of the
active flight plan.

AUDIO PANEL
& CNS

In flight plan mode (FPL) with the active flight plan selected (00), and a specific leg (NN) selected, the
‘from’ waypoint is the current aircraft position and the ‘to’ waypoint is the endpoint of the selected leg.
In waypoint (WPTS) mode these are manually selected waypoints (if there is an active flight plan, these
default to the endpoints of the active leg).

FLIGHT
MANAGEMENT

Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already
been flown.
• Desired Track (DTK) - DTK is shown as nnn° and is the desired track between the selected waypoints.
It is dashed unless only a single leg is selected.
• Distance (DIS) - The distance is shown in tenths of units up to 99.9, and in whole units up to 9999.

HAZARD
AVOIDANCE

• Estimated time enroute (ETE) - ETE is shown as hours:minutes until less than an hour, then it is shown
as minutes:seconds.
• Estimated time of arrival (ETA) - ETA is shown as hours:minutes and is the local time at the
destination.

AFCS

- If a flight plan other than the active flight plan is selected it shows the ETA by adding to the departure
time all of the ETEs of the legs up to and including the selected leg. If the entire flight plan is selected,
then the ETA is calculated as if the last leg of the flight plan was selected.

ADDITIONAL
FEATURES

- If in waypoint mode then the ETA is the ETE added to the departure time.

- If the active flight plan is selected the ETA reflects the current position of the aircraft and the current
leg being flown. The ETA is calculated by adding to the current time the ETEs of the current leg up to
and including the selected leg. If the entire flight plan is selected, then the ETA is calculated as if the
last leg of the flight plan was selected.

APPENDICES

• Enroute safe altitude (ESA) - The ESA is shown as nnnnnFT

INDEX

• Destination sunrise and sunset times (SUNRISE, SUNSET) - These times are shown as hours:minutes
and are the local time at the destination.

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Flight Management
SYSTEM
OVERVIEW

Fuel Statistics

FLIGHT
INSTRUMENTS

The fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning
inputs. Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has
already been flown.
• Fuel efficiency (EFFICIENCY) - This value is calculated by dividing the current ground speed by the
current fuel flow.
• Time of fuel endurance (TOTAL ENDUR) - This time is shown as hours:minutes. This value is obtained
by dividing the amount of fuel on board by the current fuel flow.

EIS

• Fuel on board upon reaching end of selected leg (REM FUEL) - This value is calculated by taking the
amount of fuel onboard and subtracting the fuel required for trip.

AUDIO PANEL
& CNS

• Fuel endurance remaining at end of selected leg (REM ENDUR) - This value is calculated by subtracting
the time of fuel endurance by the amount of time to go.
• Fuel required for trip (FUEL REQ) - This value is calculated by multiplying the time to go by the fuel
flow.

FLIGHT
MANAGEMENT

• Total range at entered fuel flow (TOTAL RANGE) - This value is calculated by multiplying the time of fuel
endurance by the ground speed.

Other Statistics
These statistics are calculated based on the system sensor inputs or the manual trip planning inputs.

HAZARD
AVOIDANCE

• Density altitude (DENSITY ALT)
• True airspeed (TRUE AIRSPEED)
The pilot may select automatic (AUTO) or manual (MANUAL) page mode, and flight plan (FPL) or waypoint
(WPTS) mode. In automatic page mode, only the FPL, LEG, or waypoint IDs are editable (based on FPL/WPTS
selection).

AFCS

Selected Flight Plan NN -

Selected Leg(s)

00 is Active FPL
01-99 are Stored FPLs

ADDITIONAL
FEATURES

Starting and Ending Waypoint of
Selected Flight Plan Segment

Stored Flight Plan
- CUM: Beginning to End of FPL
- NN: Beginning to End of Selected Leg
Active Flight Plan
- REM: Pres. Pos. to End of FPL
- NN: Pres. Pos. to End of Selected Leg

Figure 5-98 Trip Planning Page - Flight Plan Mode

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Flight Management
Selected Flight Plan

Selected Leg(s)

Not Available

FLIGHT
INSTRUMENTS

Selected Starting and Ending Waypoints
Figure 5-99 Trip Planning Page - Waypoint Mode

Selecting automatic or manual page mode:

EIS

Press the AUTO Softkey or the MANUAL Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual
Mode’, and press the ENT Key.

Selecting flight plan or waypoint mode:
AUDIO PANEL
& CNS

Press the FPL Softkey or the WPTS Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints
Mode’, and press the ENT Key.

Selecting a flight plan and leg for trip statistics:

FLIGHT
MANAGEMENT

1) Press the FMS Knob to activate the cursor in the flight plan number field.
2) Turn the small FMS Knob to select the desired flight plan number.
3) Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for each leg can be viewed by turning the
small FMS Knob to select the desired leg. The Inset Map also displays the selected data.

HAZARD
AVOIDANCE

Selecting waypoints for waypoint mode:
1) Press the WPTS Softkey; or press the MENU Key, highlight ‘Waypoints Mode’, and press the ENT Key. The
cursor is positioned in the waypoint field directly below the FPL field.

AFCS

2) Turn the FMS knobs to select the desired waypoint (or select from the Page Menu ‘Set WPT to Present Position’
if that is what is desired), and press the ENT Key. The cursor moves to the second waypoint field.
3) Turn the FMS knobs to select the desired waypoint, and press the ENT Key. The statistics for the selected leg
are displayed.

ADDITIONAL
FEATURES

In manual page mode, the other eight trip input data fields must be entered by the pilot, in addition to flight
plan and leg selection.
Entering manual data for trip statistics calculations:

APPENDICES

1) Press the MANUAL Softkey or select ‘Manual Mode’ from the Page Menu, and press the ENT Key. The cursor
may now be positioned in any field in the top right two boxes.

INDEX

2) Turn the FMS Knobs to move the cursor onto the DEP TIME field and enter the desired value. Press the ENT Key.
The statistics are calculated using the new value and the cursor moves to the next entry field. Repeat until all
desired values have been entered.

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OVERVIEW

5.10 RAIM Prediction

FLIGHT
INSTRUMENTS

RAIM (Receiver Autonomous Integrity Monitoring) is a GPS receiver function that performs a consistency
check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate
a position within a specified RAIM protection limit (2.0 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal,
and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is
available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a
specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival
date and time. Because of the tighter protection limit on approaches, there may be times when RAIM is not
available. RAIM prediction must be initiated manually if there is concern over WAAS coverage at the destination
or some other reason that compromises navigation precision. If RAIM is not predicted to be available for the
final approach course, the approach does not become active. If RAIM is not available when crossing the FAF, the
missed approach procedure must be flown.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

RAIM PREDICTION Box
- Prediction Waypoint
- Arrival Time
- Arrival Date
- RAIM Status

HAZARD
AVOIDANCE
AFCS

RAIM Softkey

SBAS Softkey
(displays SBAS Selection)

(displays RAIM
PREDICTION)

ADDITIONAL
FEATURES

Figure 5-100 RAIM Prediction

APPENDICES

Predicting RAIM availability at a selected waypoint:
1) Select the AUX-GPS Status Page.
2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.

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Flight Management
4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of
waypoints and press the ENT Key to accept the waypoint entry.
5) Turn the FMS Knobs to enter an arrival time and press the ENT Key.

FLIGHT
INSTRUMENTS

6) Turn the FMS Knobs to enter an arrival date and press the ENT Key.
7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation.

Predicting RAIM availability at the aircraft present position:
1) Select the AUX-GPS Status Page.

EIS

2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.
3) Press the MENU Key, highlight ‘Set WPT to Present Position’, and press the ENT Key.

AUDIO PANEL
& CNS

4) Press the ENT Key to accept the waypoint entry.
5) Turn the FMS Knobs to enter an arrival time and press the ENT Key.
6) Turn the FMS Knobs to enter an arrival date and press the ENT Key.

FLIGHT
MANAGEMENT

Status of the RAIM computation for the selected waypoint, time, and date is displayed at the bottom of the
RAIM PREDICTION Box as follows:

HAZARD
AVOIDANCE

7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation.

• ‘RAIM AVAILABLE’ - RAIM is predicted to be available.

• ‘COMPUTE RAIM?’ - RAIM has not been computed.
• ‘COMPUTING AVAILABILITY’ - RAIM calculation is in progress.
• ‘RAIM NOT AVAILABLE’ - RAIM is predicted to be unavailable.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

The Satellite Based Augmentation System (SBAS) provides increased navigation accuracy when available. SBAS
can be enabled or disabled manually on the GPS Status Page.

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Flight Management
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

SBAS Status

SBAS SELECTION Box

- MSAS Enable/Disable
- WAAS Enable/Disable

EIS
AUDIO PANEL
& CNS

RAIM Softkey

SBAS Softkey
(displays SBAS Selection)

(displays RAIM
PREDICTION)

FLIGHT
MANAGEMENT

Figure 5-101 SBAS Display - Active

Enabling/Disabling SBAS:

HAZARD
AVOIDANCE

1) Select the AUX-GPS Status Page.
2) Press the FMS Knob, and turn the large FMS Knob to highlight ‘MSAS’ or ‘WAAS’.
3) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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FLIGHT
INSTRUMENTS

SBAS Status

SBAS SELECTION Box

AUDIO PANEL
& CNS

EIS

- MSAS Enable/Disable
- WAAS Enable/Disable

RAIM Softkey

SBAS Softkey
(displays SBAS Selection)

FLIGHT
MANAGEMENT

(displays RAIM
PREDICTION)

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Figure 5-102 SBAS Display - Disabled

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OVERVIEW

5.11 Navigating a Flight Plan

FLIGHT
INSTRUMENTS

The following discussion is an example of navigating a flight plan with the WAAS capable GPS system while the
G1000 provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the
same way, but would not include vertical guidance when the final approach course is active.
nOTE: The following example flight plan is for instructional purposes only. All database information depicted

should be considered not current.

EIS

The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure, various Victor Airways,
and the DBRY1 arrival with the transition at TBE. The flight plan includes an enroute altitude of 12,000 feet, an
LPV (WAAS) approach selected for runway 35R, and a missed approach executed at the Missed Approach Point
(MAP). A few enroute changes are demonstrated.

AUDIO PANEL
& CNS

1) Prior to departure, the TIFTO2 departure, the airways, and the DBRY1 arrival at KCOS are loaded. See the
Procedures section for loading departures and arrivals. Note the magenta arrow in Figure 5-103 indicating the
active departure leg.

After takeoff, ATC assigns a heading of 240º.

FLIGHT
MANAGEMENT

2) Figure 5-103 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI flight
phase displayed on the HSI indicating 1.0 nm CDI scaling.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-103 Assigned Heading of 240º

INDEX

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FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading
290° as seen in Figure 5-104.

Figure 5-104 Assigned Heading of 290º

HAZARD
AVOIDANCE

4) Enter V4 into the flight plan.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

a) Press the FMS Knob to activate the cursor.

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OVERVIEW

b) The desired entry point for V4 (TOP) must be entered. Turn the large FMS Knob to highlight the desired flight
plan insertion point (SLN) as shown in Figure 5-105. When the V4 entry point (TOP) is inserted, it is placed
immediately above the highlighted waypoint (SLN).

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-105 Begin Adding V4 to the Flight Plan

c) Turn the small FMS Knob to display the Waypoint Information Window. Enter the desired entry point for V4,
Topeka VOR (TOP), as shown in Figure 5-106.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-106 Entering V4 Entry Point

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OVERVIEW

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AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 5-107.

FLIGHT
MANAGEMENT

Figure 5-107 TOP Inserted into the Flight Plan

e) With SLN still highlighted as in Figure 5-104, turn the small FMS Knob clockwise. The Waypoint Information
Page is displayed and the LD AIRWY Softkey is now available.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-108.

APPENDICES

Figure 5-108 List of Available Airways for TOP

INDEX

g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 5-108.

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OVERVIEW

h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-109.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

Figure 5-109 List of Available Exits for V4

FLIGHT
MANAGEMENT

i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as in
Figure 5-109.
j) Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in
Figure 5-110.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-110 Ready to Load V4

k) Press the ENT Key.

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OVERVIEW

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AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

l) V4 is now loaded into the flight plan as shown in Figure 5-111.

FLIGHT
MANAGEMENT

Figure 5-111 V4 is Loaded in the Flight Plan

5) Making V4 the active leg of the flight plan.
a) Press the FMS Knob to activate the cursor.

HAZARD
AVOIDANCE

b) Turn the large FMS Knob to highlight ULNAZ. The TO waypoint of the leg is selected in order to activate the
leg.

AFCS

c) Press the ACT LEG Softkey. The confirmation window is now displayed as in Figure 5-112. Note the TOP to
ULNAZ leg is actually part of V4.

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 5-112 Comfirm Active Leg

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SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-113, the magenta arrow in
the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the
phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active. Since a
leg after the departure is now active, the current CDI flight phase is ENR (Enroute) and CDI scaling has changed
to 2.0 nm.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 5-113 V4 Now Active Leg

6) The aircraft continues on heading 290º. When crosstrack distance is less than 2.0 nm, the XTK disappears from
the HSI and the CDI is positioned on the last dot indicating a 2.0 nm distance from the centerline of the next
course.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

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FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 5-114.

Figure 5-114 Turn on to Active Leg

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box
as seen in Figure 5-115.

INDEX

APPENDICES

Figure 5-115 Turn to Intercept V244

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OVERVIEW

9) As seen in Figure 5-116, V244 is now the active flight plan leg.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-116 V244 Now Active Leg

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

Flight Management

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-117.

Figure 5-117 HYS to LAA Legs Active

HAZARD
AVOIDANCE

11) ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure. ATC advises
to expect an altitude of 10,000 feet at OPSHN.
a) Press the FMS Knob to activate the cursor.
b) Turn the large FMS Knob to select OPSHN in the flight plan list.
) Key. The Direct-to Window is now displayed as shown in Figure 5-118.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

c) Press the Direct-to (

Figure 5-118 Direct To OPSHN

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OVERVIEW

d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-119.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-119 Enter VNV Altitude

e) An altitude of 10,000 feet is entered as requested by ATC.
f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 5-120.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-120 Enter VNV Offset Distance

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INDEX

g) Enter the offset, or distance from the waypoint at which to reach the selected altitude. In this case, three miles
prior to OPSHN is entered. In other words, the G1000 gives vertical guidance so the aircraft arrives at an
altitude of 10,000 feet three miles prior to OPSHN.

257

SYSTEM
OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-121, the magenta arrow indicating the directto OPSHN after the offset waypoint for OPSHN. The preceding offset waypoint indicates the offset distance
and altitude that were previously entered. The remaining waypoints in the loaded arrival procedure have no
database specified altitudes, therefore, dashes are displayed. Keep the CDI centered and maintain a track along
the magenta line to OPSHN.
Note the Direct-to waypoint is within the loaded arrival procedure, therefore, phase of flight scaling for the CDI
changes to Terminal Mode and is annunciated by displaying ‘TERM’ on the HSI.
NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

to be used as is, the altitude must be manually accepted by placing the cursor over the desired altitude,
then pressing the ENT Key. The altitude is now displayed as light blue meaning it is used by the system to
determine vertical speed and deviation guidance.

ADDITIONAL
FEATURES

Figure 5-121 Direct-to Active

12) The aircraft is proceeding to OPSHN. The expected approach is the RNAV LPV approach to runway 35R, so it is
selected.

INDEX

APPENDICES

a) Press the PROC Key to display the Procedures Window.

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OVERVIEW

b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-122.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-122 Proceudures Window

c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-123.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-123 List of Available Approaches

d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-1201.
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AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-124.

FLIGHT
MANAGEMENT

Figure 5-124 List of Available Transitions

f) Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is
used.
g) Press the ENT Key.

HAZARD
AVOIDANCE

h) Barometric Minimums
To set MINIMUMS’, turn the small FMS Knob to select ‘BARO’, and press the ENT Key. Turn the small
FMS Knob to select the altitude, and press the ENT Key.
Or:

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

To skip setting minimums, press the ENT Key.

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OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

Figure 5-125 Barometric Minimums Set

FLIGHT
MANAGEMENT

i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen
in Figure 5-126.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-126 Loaded Approach

INDEX

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13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-127. These
altitudes are loaded from the database and are displayed as light blue text, indicating these values are
“designated” for use in computing vertical deviation guidance.

EIS

FLIGHT
INSTRUMENTS

Note: To no longer use the displayed altitude for calculating vertical deviation guidance, perform the
following:

a) Press the FMS Knob to activate the cursor.

b) Turn the small FMS Knob to highlight the desired altitude.

c) Press the CLR Key.

d) Press the FMS Knob to deactivate the cursor.

After making the altitude “non-designated”, it is displayed as white text.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be
designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 5-127.
Vertical guidance from the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS
altitude source, therefore, the displayed altitude values are for reference only.

INDEX

APPENDICES

Figure 5-127 Vertical Guidance is Active to the FAF

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OVERVIEW

14) As the aircraft approaches OPSHN, it may be desirable to adjust the speed, or steepness of the upcoming
descent. The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to
maintain the -3.0 FPA. To change the vertical flight path, perform the following steps.

FLIGHT
INSTRUMENTS

a) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure
5-128.
b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob
to select the desired selection field, then turn the small FMS Knob to enter the desired value.

EIS

Note the information now displayed in the ‘CURRENT VNV PROFILE’ box. Also, note the offset waypoint (orange
box) and gray circle are now displayed on the map. The gray circle marks the Top of Descent (TOD). In this
example, vertical guidance is provided at the TOD that results in a -3.0 degree FPA descent to an altitude of
10,000 feet upon reaching the offset waypoint.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

Figure 5-128 Adjusting the Descent

ADDITIONAL
FEATURES

c) Press the ENT Key.

APPENDICES
INDEX

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OVERVIEW

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FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

15) As seen in Figure 5-129, the aircraft is approaching TOD. Note the target vertical speed required to reached
the selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are
now displayed on the PFD as shown in Figure 5-130. When the aircraft is within one minute of the TOD, it is
annunciated as shown in Figure 5-130, and an aural alert ‘Vertical track’ will be heard.

HAZARD
AVOIDANCE

Figure 5-129 Approaching Top of Descent (TOD)

AFCS

Target Altitude

ADDITIONAL
FEATURES

Vertical Deviation
Indicator (VDI)

APPENDICES

Required Vertical
Speed Indicator
(RVSI)

INDEX

Figure 5-130 VDI & RVSI Upon Reaching Top of Descent (TOD)

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SYSTEM
OVERVIEW

16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as
shown in Figure 5-131.

FLIGHT
INSTRUMENTS
EIS

Keep Vertical Deviation
Indicator Centered

AUDIO PANEL
& CNS

Align Actual Vertical Speed
with
Required Vertical Speed

FLIGHT
MANAGEMENT

Figure 5-131 VDI & RVSI Showing Correctly Established Descent

17) When the aircraft is one minute from the bottom of descent (BOD) it is annunciated as shown in Figure 5-132.
Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet.

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-132 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint

INDEX

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SYSTEM
OVERVIEW

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AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the
PFD as seen in Figure 5-133. Initiate the turn and maneuver the aircraft on a track through the turn radius to
intercept the magenta line for the OPSHN to FSHER leg and center the CDI.

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 5-133 Turn to intercept OPSHN to FSHER Leg

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SYSTEM
OVERVIEW

19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-134. The magenta arrow
in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-134 Tracking the OPSHN to FSHER Leg

HAZARD
AVOIDANCE

20) The flight continues through the arrival procedure to PYNON (see Figure 5-135). At a point 31 nm from the
destination airport, the phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by
displaying ‘TERM’ on the HSI.
A descent to HABUK is in the next leg. Note the TOD point on the map. Annunciations for the upcoming turn
and descent, as well as the VDI and RVSI, appear on the PFD as the flight progresses.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Flight Management

INDEX

Figure 5-135 Approaching PYNON

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SYSTEM
OVERVIEW

21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated
at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final
waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating
the approach procedure (see Figure 5-136).

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-136 Approach is Now Active

HAZARD
AVOIDANCE

Note: To manually activate the approach procedure, perform the following steps:
a) Press the PROC Key.
b) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’ as shown in Figure 5-137.

AFCS

c) Press the ENT Key to activate the approach.

ADDITIONAL
FEATURES
APPENDICES

Figure 5-137 Manually Activate Approach

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Flight Management

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16.
The aircraft altitude is 9,000 feet upon reaching HABUK.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Figure 5-138 Descending Turn to the Initial Approach Fix (IAF)

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SYSTEM
OVERVIEW

23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the
current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is
used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to
the Glidepath Indicator (as shown in Figure 5-139) when the final approach course becomes active.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 5-139 Descending to the FAF

HAZARD
AVOIDANCE

The descent continues through the FAF (CEGIX) using the Glidepath Indicator, as one would use a glideslope
indicator, to obtain an altitude “AT” 7,800 feet at the FAF. Note the altitude restriction lines over and under (At)
the altitude in the ‘ALT’ field in Figure 5-139.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

Flight Management

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to “AT or ABOVE”
6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 5-140.

Figure 5-140 Descending to the Missed Approach Point

AFCS

HAZARD
AVOIDANCE

In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part
of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway
centerline until the altitude required to safely make the first turn toward the MAHP is exceeded. This altitude
is provided by Jeppesen, and may be below, equal to, or above the published minimums for this approach. In
this case, if the aircraft altitude is below the specified altitude (6,368 feet) after crossing the MAP, a direct-to
is established to provide a course on runway heading until an altitude of 6,368 feet is reached. After reaching
6,368 feet, a direct-to is established to the published MAHP (in this case MOGAL). If the aircraft altitude is
above the specified altitude after crossing the MAP, a direct-to is established to the published fix (MOGAL) to
begin the missed approach procedure.

INDEX

APPENDICES

ADDITIONAL
FEATURES

In some missed approach procedures this Course to Altitude leg may be part of the published procedure. For
example, a procedure may dictate a climb to 5,500 feet, then turn left and proceed to the Missed Approach Hold
Point (MAHP). In this case, the altitude would appear in the list of waypoints as ‘5500ft’. Again, if the aircraft
altitude is lower than the prescribed altitude, a direct-to is established on a Course to Altitude leg when the
missed approach procedure is activated.

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SYSTEM
OVERVIEW

25) Upon reaching the MAP, it is decided to execute a missed approach. Automatic waypoint sequencing is
suspended past the MAP. Press the SUSP Softkey on the PFD to resume automatic waypoint sequencing
through the missed approach procedure.

FLIGHT
INSTRUMENTS

A direct-to is initiated to MOGAL, which is the Missed Approach Hold Point (MAHP) as seen in Figure 5-141.
The aircraft is climbing to 10,000 feet. The CDI flight phase now changes from LPV to MAPR as seen on the
HSI.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 5-141 Missed Approach Active

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FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at
the MAHP (MOGAL) as shown in Figure 5-142.

Figure 5-142 Establishing the Holding Pattern

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-143.

INDEX

Figure 5-143 Hold Established

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OVERVIEW

5.12 Abnormal Operation
This section discusses the Dead Reckoning mode of operation and the subsequent indications.

FLIGHT
INSTRUMENTS

Note: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other

phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the G1000
stops using GPS.

EIS

While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS solution or is unable to
calculate a GPS position, the system automatically reverts to Dead Reckoning (DR) Mode. In DR Mode, the G1000
uses its last-known position combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.

AUDIO PANEL
& CNS

It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly
unreliable and must not be used as a sole means of navigation. If while in DR Mode airspeed and/or heading data
is also lost or not available, the DR function may not be capable of accurately tracking estimated position and,
consequently, the system may display a path that is different than the actual movement of the aircraft. Estimated
position information displayed by the G1000 through DR while there is no heading and/or airspeed data available
should not be used for navigation.

FLIGHT
MANAGEMENT

DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the lack of satellite measurements
needed to determine a position. Changes in wind speed and/or wind direction compounds the relative inaccuracy
of DR Mode. Because of this degraded accuracy, other navigation equipment must be relied upon for position
awareness until GPS-derived position data is restored.

HAZARD
AVOIDANCE

DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own
aircraft’ symbol as shown in Figure 5-144. In addition, ‘DR’ is prominently displayed in yellow on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in Figure 5-144. Also, the CDI deviation bar
is removed from the display. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message appears on the PFD.
Normal navigation using GPS/WAAS source data resumes automatically once a valid GPS solution is restored.

AFCS

As a result of operating in DR Mode, all GPS-derived data is computed based upon an estimated position and
is displayed as yellow text on the display to denote degraded navigation source information as shown in Figure
5-144.

ADDITIONAL
FEATURES

Also, while the G1000 is in DR Mode, the autopilot does not couple to GPS, and both TAWS and Terrain SVS are
disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable.
Finally, airspace alerts continue to function, but with degraded accuracy.

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Flight Management

FLIGHT
INSTRUMENTS

Distance &
Bearing

EIS

Dead Reckoning
Annunciaion
Wind Data
GPS Navigation
Lost Message

AUDIO PANEL
& CNS

Current
Track
Indicator

FLIGHT
MANAGEMENT

Bearing
Pointer/
Distance
Wind Data

Nav Data Bar

HAZARD
AVOIDANCE

All data except
Active Leg,
TAS, and DTK
are in yellow

AFCS

Dead Reckoning
Annunciation

ADDITIONAL
FEATURES

Subdued Aircraft
Symbol

APPENDICES

Figure 5-144 Dead Reckoning Mode - GPS Derived Data Shown in Yellow

Note: The Inset Map is removed from the PFD any time aircraft pitch is greater than +30° or less than –20°,

INDEX

or when a 65° bank angle is reached.

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SYSTEM
OVERVIEW

Section 6 Hazard Avoidance

FLIGHT
INSTRUMENTS

Hazard avoidance features available for the G1000 are designed to aid situational awareness and provide advisory
information with regard to potential hazards to flight safety associated with weather, terrain, and air traffic.
Weather
• GDL 69A XM® Satellite Weather (Optional)
• L-3 STORMSCOPE® WX-500 Series II Weather Mapping Sensor (Optional)
Terrain Avoidance

EIS

• Terrain Proximity
• TERRAIN-SVS (Standard with SVS Option)

AUDIO PANEL
& CNS

• Terrain Awareness and Warning System (TAWS) (Optional)
Traffic
• TIS (Traffic Information Service)
• Avidyne TAS600® Traffic Advisory System (Optional)

FLIGHT
MANAGEMENT

6.1 XM Satellite Weather

HAZARD
AVOIDANCE

Note: XM Satellite Weather data provides information for avoiding hazardous weather. Do not utilize XM

Weather information to penetrate hazardous weather.
Note: XM Lightning and optional L-3 STORMSCOPE® WX-500 Lightning are mutually exclusive.

AFCS

XM Satellite Weather is provided through the GDL 69A, a remote-mounted data-link satellite receiver. Received
graphical weather information and associated text is displayed on the Multi Function Display (MFD) and the
Primary Flight Display (PFD) Inset Map. The GDL 69A can also receive XM Satellite Radio® entertainment
services. Both weather data and entertainment programming operate in the S-band frequency range to provide
continuous reception capabilities at any altitude throughout North America.

ADDITIONAL
FEATURES

XM Satellite Radio services are subscription-based. For more information on specific service packages, visit
www.xmradio.com.

APPENDICES
INDEX

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Hazard Avoidance

Activating Services

FLIGHT
INSTRUMENTS

Before XM Satellite Weather can be used, the service must be activated. Service is activated by providing XM
Satellite Radio with coded IDs unique to the installed GDL 69A. XM Satellite Radio and XM Satellite Weather
services each have coded IDs. The Data and Audio Radio IDs must be provided to XM Satellite Radio to activate
the weather service and entertainment subscriptions, respectively. These IDs are located on:
• The label on the back of the Data Link Receiver
• The XM Information Page on the MFD (Figure 6-1)

EIS

• The XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N
190-00355-04)
Contact the installer if the Audio and Data Radio IDs cannot be located.

AUDIO PANEL
& CNS

XM Satellite Radio uses the coded IDs to send an activation signal that allows the G1000 to display weather
data and/or entertainment programming provided through the GDL 69A.
Activating XM Satellite Weather and XM Satellite Radio services:

FLIGHT
MANAGEMENT

1) Contact XM Satellite Radio by email (address listed on their website, www.xmradio.com) or by the customer
service phone number listed on the website. Follow the instructions provided by XM Satellite Radio services.
2) Select the XM page in the Auxiliary Page Group.
3) Press the INFO Softkey to display the XM Information Page.
4) Verify that the desired services are activated.

HAZARD
AVOIDANCE

5) Press the LOCK Softkey.
6) Turn the large FMS Knob to highlight ‘YES’.
7) To complete activation, press the ENT Key.
Audio Radio ID
(for XM
Satellite Radio)

ADDITIONAL
FEATURES

AFCS

Data Radio ID
(for XM Weather)

APPENDICES

Weather
Products
(Available
Products for
Service Class
Indicated in
Green)

INDEX

Select to Display XM
Information page

278

Figure 6-1 XM Information Page

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

Select to Lock
Subscription
Information

190-00592-06 Rev. A

Hazard Avoidance
SYSTEM
OVERVIEW

Using XM Satellite Weather Products
The primary map for viewing XM Weather data is the Weather Data Link Page in the Map Page Group. This
is the only G1000 map display capable of showing information for all available XM weather products.

FLIGHT
INSTRUMENTS

Viewing the Weather Data Link Page:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Weather Data Link Page.

EIS

NEXRAD Weather
Product Age

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

NEXRAD
Weather
Product
Selected for
Display

NEXRAD Weather
Product Display
Enabled

Figure 6-2 Weather Data Link Page
AFCS
ADDITIONAL
FEATURES

When a weather product is active on the Weather Data Link Page or the Navigation Map Page, the age of the
data is displayed on the screen (Figure 6-2). The age of the product is based on the time difference between
when the data was assembled on the ground and the current GPS time. Weather products are refreshed at
specific intervals (defined in the Refresh Rate column in Table 6-1).
If for any reason, a weather product is not refreshed within the 30-, 60-, 90-, or 180 minute Expiration Time
intervals (see Table 6-1), the data is considered expired and is removed from the display. This ensures that the
displayed data is consistent with what is currently being broadcast by XM Satellite Radio services. If more than
half of the expiration time has elapsed, the color of the product age displayed changes to yellow.

APPENDICES

Table 6-1 shows the weather product symbols, the expiration time and the refresh rate. The refresh rate
represents the interval at which XM Satellite Radio broadcasts new signals that may or may not contain new
weather data. It does not represent the rate at which weather data is updated or new content is received by
the Data Link Receiver. Weather data is updated at intervals that are defined and controlled by XM Satellite
Radio and its data vendors.

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Hazard Avoidance
Expiration Time
(Minutes)
30

Refresh Rate
(Minutes)
5

Cloud Top (CLD TOP)

Echo Top (ECHO TOP)

7.5

XM Lightning (LTNG)

Cell Movement (CELL MOV)

1.25

SIGMETs/AIRMETs (SIG/AIR)

METARs

City Forecast (CITY)

Surface Analysis (SFC)

Freezing Levels (FRZ LVL)

Winds Aloft (WIND)

County Warnings (COUNTY)

Cyclone Warnings (CYCLONE)

180

30
60
60

5
12
12

Weather Product

Symbol

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

NEXRAD

INDEX

APPENDICES

ADDITIONAL
FEATURES

Icing Potential (CIP and SLD)
(ICNG)
Pilot Weather Report
(PIREPs)
Air Report
(AIREPs)
Turbulence
(TURB)
Radar Coverage
TFRs
TAFs

No product image
No product image
No product image

Table 6-1 Weather Product Symbols and Data Timing

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SYSTEM
OVERVIEW

Echo Top (ECHO TOP)

Flight Plan Pages

Cell Movement (CELL MOV)

SIGMETs/AIRMETs (SIG/AIR)

METARs

City Forecast (CITY)

Surface Analysis (SFC)

Freezing Levels (FRZ LVL)

Winds Aloft (WIND)

County Warnings (COUNTY)

Cyclone Warnings (CYCLONE)

Icing Potential (ICNG)

PIREPs

AIREPs

Turbulence (TURB)

+
+

ADDITIONAL
FEATURES

TAFs

AFCS

TFRs

HAZARD
AVOIDANCE

Radar Coverage

FLIGHT
MANAGEMENT

XM Lightning (LTNG)

AUDIO PANEL
& CNS

Cloud Top (CLD TOP)

Nearest Page Group

AUX - Trip Planning
Page

Weather Data Link
Page

Weather Information
Page

Navigation Map Page

EIS

NEXRAD

FLIGHT
INSTRUMENTS

Weather Product

PFD Inset Map

Table 6-2 shows which XM products can be displayed (indicated with a ‘+’ symbol) on specific maps.

APPENDICES

Table 6-2 Weather Product Display Maps

INDEX

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Hazard Avoidance

FLIGHT
INSTRUMENTS

Softkeys control the display of weather information on most MFD pages and the PFD Inset Map (Figure 6-3
shows the weather product softkeys for the Weather Data Link Page). When a weather product is selected
for display, the corresponding softkey label changes to gray to indicate the product is enabled. Unavailable
weather products have subdued softkey labels (softkeys are disabled from selection).
NEXRAD ECHO TOP CLD TOP

ENGINE

CYCLONE SFC OFF

FRZ LVL

SIG/AIR

METAR

LEGEND MORE WX CHKLIST

WIND OFF ICNG OFF TURB OFF AIREPS

PIREPS

COUNTY

LTNG

CELL MOV

BACK

EIS

SFC Softkey label changes
to reflect current selection.
WIND/ICNG/TURB Softkey labels
change to reflect current selection.
CURRENT

AUDIO PANEL
& CNS

OFF

12 HR

24 HR

36 HR

48 HR

Select the BACK Softkey
to move up one level.
LEGEND

BACK

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

PREV and NEXT Softkeys cycle through Winds Aloft,
Icing, and Turbulence altitude selection softkeys.
PREV

OFF

SFC

3000

6000

9000

12000

15000

LEGEND

BACK

OFF

18000

21000

24000

27000

30000

33000

LEGEND

BACK

OFF

36000

39000

42000

LEGEND

BACK

OFF

1000

3000

6000

9000

12000

LEGEND

BACK

OFF

18000

21000

24000

27000

30000

LEGEND

BACK

OFF

21000

24000

27000

30000

33000

LEGEND

BACK

OFF

39000

42000

45000

LEGEND

BACK

15000

36000

Figure 6-3 Weather Data Link Weather Product Softkeys

INDEX

APPENDICES

The setup menus for the Navigation Map Page and the Weather Data Link Page control the map range settings
above which weather products data are decluttered from the display. If a map range larger than the weather
product map range setting is selected, the weather product data is removed from the map. The menus also
provide a means in addition to the softkeys for enabling/disabling display of weather products.

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SYSTEM
OVERVIEW

Setting up and customizing the Weather Data Link Page:
1) Select the Weather Data Link Page.
2) Press the MENU Key.

FLIGHT
INSTRUMENTS

3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-4).
4) Turn the small FMS Knob to select ‘XM Product Group 1’ or ‘XM Product Group 2’, and press the ENT Key
(Figure 6-5).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections.

EIS

6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.).
7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Weather Data Link Page with the changed settings.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 6-4 Weather Data Link Page Menu

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Figure 6-5 Weather Data Link Page Setup Menu

Restoring default Weather Data Link Page settings:
1) Select the Weather Data Link Page.

APPENDICES

2) Press the MENU Key.
3) With ‘Weather Setup’ highlighted, press the ENT Key.
4) Press the MENU Key.
5) Highlight the desired default(s) to restore (all or for selection) and press ENT Key.

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OVERVIEW

Hazard Avoidance
Maps besides the Weather Data Link Page use settings based on those selected for the Navigation Map Page.
Setting up and customizing weather data for the Navigation Map Page:

FLIGHT
INSTRUMENTS

1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-6).
4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key (Figure 6-7).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-8).

EIS

6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

ADDITIONAL
FEATURES

AFCS

Figure 6-6 Navigation Map Page Menu

Figure 6-8 Navigation Map Page Setup Menu, Weather Group

INDEX

APPENDICES

Figure 6-7 Navigation Map Page Setup Menu

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SYSTEM
OVERVIEW

Each active weather product has an associated legend which can be displayed on the Weather Data Link
Page.
Viewing legends for displayed weather products

FLIGHT
INSTRUMENTS

1) Select the Weather Data Link Page.
2) Press the LEGEND Softkey to display the legends for the displayed weather products.
Or:

a) Press the MENU Key.
b) Select ‘Weather Legend’ and press the ENT Key.
EIS

3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window.
4) To remove the Legend Window, press the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob.

• County Warnings

• Cell Movement

• TFRs

• SIGMETs

• AIREPs

• AIRMETs

• PIREPs

FLIGHT
MANAGEMENT

• Echo Tops

AUDIO PANEL
& CNS

Additional information about the following can be displayed by panning over the display on the map:

• METARs

HAZARD
AVOIDANCE

The map panning feature is enabled by pressing the RANGE Knob. The map range is adjusted by turning
the RANGE Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map
Pointer.
Additional
Information on
Weather Feature
Selected with
Map Pointer

AFCS
ADDITIONAL
FEATURES

Flash Flood
Warning
Selected with
Map Pointer

APPENDICES
INDEX

Figure 6-9 Panning on the Weather Data Link Page

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SYSTEM
OVERVIEW

NEXRAD

FLIGHT
INSTRUMENTS

Hazard Avoidance

WSR-88D, or NEXRAD (NEXt-generation RADar), is a network of 158 high-resolution Doppler radar
systems that are operated by the National Weather Service (NWS). NEXRAD data provides centralized
meteorological information for the continental United States and selected overseas locations. The maximum
range of a single NEXRAD radar site is 250 nm. In addition to a wide array of services, the NEXRAD network
provides important information about severe weather and air traffic safety.

NOTE: NEXRAD cannot be displayed at the same time as terrain.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

NEXRAD data is not real-time. The lapsed time between collection, processing, and dissemination of
NEXRAD images can be significant and may not reflect the current radar synopsis. Due to the inherent delays
and the relative age of the data, it should be used for long-range planning purposes only. Never use NEXRAD
data or any radar data to penetrate hazardous weather. Rather, use it in an early-warning capacity of predeparture and enroute evaluation.

Figure 6-10 NEXRAD Data on the Weather Data Link Page

APPENDICES

NEXRAD data can be displayed on the following maps:
• PFD Inset Map

• Trip Planning Page

• Navigation Map Page

• Nearest Pages

• Weather Data Link Page

• Flight Plan Pages

INDEX

• Airport Information Page

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SYSTEM
OVERVIEW

Displaying NEXRAD weather information:
1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the
Weather Data Link Page.

FLIGHT
INSTRUMENTS

2) Press the NEXRAD Softkey.

Composite data from all the NEXRAD radar sites in the United States is shown. This data is composed of
the maximum reflectivity from the individual radar sweeps. The display of the information is color-coded to
indicate the weather severity level. All weather product legends can be viewed on the Weather Data Link Page.
For the NEXRAD legend (Figure 6-11), press the LEGEND Softkey when NEXRAD is selected for display.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

No Radar Coverage
Figure 6-11 NEXRAD Data with Legend

HAZARD
AVOIDANCE

The display of radar coverage is always active when either NEXRAD or ECHO TOPS is selected. Areas
where NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected
are indicated in grayish-purple. Radar capability exists in these areas, but it is not active or is off-line.

Reflectivity

AFCS

Reflectivity is the amount of transmitted power returned to the radar receiver. Colors on the NEXRAD
display are directly correlative to the level of detected reflectivity. Reflectivity as it relates to hazardous
weather can be very complex.

ADDITIONAL
FEATURES

The role of radar is essentially to detect moisture in the atmosphere. Simply put, certain types of weather
reflect radar better than others. The intensity of a radar reflection is not necessarily an indication of the
weather hazard level. For instance, wet hail returns a strong radar reflection, while dry hail does not. Both
wet and dry hail can be extremely hazardous.

APPENDICES

The different NEXRAD echo intensities are measured in decibels (dB) relative to reflectivity (Z). NEXRAD
measures the radar reflectivity ratio, or the energy reflected back to the radar receiver (designated by the
letter Z). The value of Z increases as the returned signal strength increases.

INDEX

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OVERVIEW

Hazard Avoidance
NEXRAD Limitations
NEXRAD radar images may have certain limitations:

FLIGHT
INSTRUMENTS

• NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation
characteristics (wet hail vs. rain). For example, it is not possible to distinguish between wet snow, wet
hail, and rain.
• NEXRAD base reflectivity is sampled at the minimum antenna elevation angle. An individual NEXRAD
site cannot depict high altitude storms at close ranges. It has no information about storms directly over
the site.

AUDIO PANEL
& CNS

EIS

• When zoomed in to a range of 30 nm, each square block on the display represents an area of four square
kilometers. The intensity level reflected by each square represents the highest level of NEXRAD data
sampled within the area (Figure 6-12).

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Block Area is 4 km2

Figure 6-12 NEXRAD Data - Zoomed
ADDITIONAL
FEATURES

The following may cause abnormalities in displayed NEXRAD radar images:
• Ground clutter
• Strobes and spurious radar data

APPENDICES

• Sun strobes (when the radar antenna points directly at the sun)
• Interference from buildings or mountains, which may cause shadows

INDEX

• Metallic dust from military aircraft, which can cause alterations in radar scans

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SYSTEM
OVERVIEW

NEXRAD Limitations (Canada)
• Radar coverage extends to 55ºN.

FLIGHT
INSTRUMENTS

• Any precipitation displayed between 52ºN and 55ºN is displayed as mixed because it is unknown.
No Coverage Above 55ºN

EIS
AUDIO PANEL
& CNS

Precipitation
Above 52ºN

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 6-13 NEXRAD Data - Canada

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

ECHO TOPs

FLIGHT
INSTRUMENTS

Hazard Avoidance

Echo Tops data (Figure 6-14) shows the location, elevation, and direction of the highest radar echo. The
highest radar echo does not indicate the top of a storm or clouds; rather it indicates the highest altitude at
which precipitation is detected. Information is derived from NEXRAD data.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Note: Display of Echo Tops is mutually exclusive with Cloud Tops and NEXRAD.

Figure 6-14 Echo Tops Data

AFCS

Displaying Echo Tops information:
1) Select the Weather Data Link Page.
2) Press the ECHO TOP Softkey.

APPENDICES

ADDITIONAL
FEATURES

To display the Echo Tops legend (Figure 6-15), press the LEGEND Softkey when Echo Tops is selected for
display. Since Echo Tops and Cloud Tops use the same color scaling to represent altitude, display of these
weather products is mutually exclusive. When Echo Tops is activated, NEXRAD and Cloud Tops data are
removed.

INDEX

No Radar Coverage
Figure 6-15 ECHO TOPS Legend

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SYSTEM
OVERVIEW

FLIGHT
INSTRUMENTS

Cloud TOPs
Note: Cloud Tops and Echo Tops cannot be displayed at the same time.

Cloud Tops data (Figure 6-16) depicts cloud top altitudes as determined from satellite imagery.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 6-16 Cloud Tops Data
AFCS

Displaying Cloud Tops information:
1) Select the Weather Data Link Page.

ADDITIONAL
FEATURES

2) Press the CLOUD TOPS Softkey.

To display the Cloud Tops legend (Figure 6-17), press the LEGEND Softkey when Cloud Tops is selected for
display. Since Cloud Tops and Echo Tops use the same color scaling to represent altitude, display of these
weather products is mutually exclusive. When Cloud Tops is activated, Echo Tops data is removed.

APPENDICES
INDEX

Figure 6-17 Cloud Tops Legend

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OVERVIEW

Hazard Avoidance
XM Lightning
Note: L-3 STORMSCOPE® WX-500 Lightning and GDL 69/69A XM® Satellite Weather Lightning are

FLIGHT
INSTRUMENTS

mutually exclusive.

AUDIO PANEL
& CNS

EIS

Lightning data (Figure 6-18) shows the approximate location of cloud-to-ground lightning strikes. A strike
icon represents a strike that has occurred within a two-kilometer region. The exact location of the lightning
strike is not displayed.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Lightning
Strikes

Figure 6-18 Lightning Data

ADDITIONAL
FEATURES

AFCS

XM Lightning data displays on the following maps:
• PFD Inset Map

• Trip Planning Page

• Navigation Map Page

• Nearest Pages

• Weather Data Link Page

• Flight Plan Pages

Displaying XM Lightning information:

APPENDICES

1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the
Weather Data Link Page.
2) Press the XM LTNG Softkey (LTNG Softkey on the Weather Data Link Page).

INDEX

To display the XM Lightning legend on the Weather Data Link Page (Figure 6-19), press the LEGEND Softkey
when XM Lightning is selected for display.

Figure 6-19 Lightning Legend

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SYSTEM
OVERVIEW

Cell Movement

FLIGHT
INSTRUMENTS

Cell Movement data (Figure 6-20) shows the location and movement of storm cells as identified by the
ground-based system. Cells are represented by yellow squares, with direction of movement indicated with
short, orange arrows.

EIS
AUDIO PANEL
& CNS

Storm Cells

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 6-20 Cell Movement Data

On most applicable maps, Cell Movement data is selected for display along with NEXRAD. On the Weather
Data Link Page, Cell Movement data can be selected independently. Cell Movement data can be displayed
on the following maps:
• AUX - Trip Planning Page

•Navigation Map

• Nearest Pages

AFCS

• PFD Inset Map

Displaying Cell Movement information:
ADDITIONAL
FEATURES

1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the
Weather Data Link Page.

APPENDICES

2) Press the NEXRAD Softkey (CEL MOV Softkey on the Weather Data Link Page). For Cell Movement to be
displayed on maps other than the Weather Data Link Page, Cell Movement must be turned on in the Navigation
Map Setup Menu (see “Setting Up XM Satellite Weather”).

To display the Cell Movement legend on the Weather Data Link Page, (Figure 6-21), press the LEGEND
Softkey when Cell Movement is selected for display.

INDEX

Figure 6-21 Cell Movement Legend

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Hazard Avoidance
SIGMETS and AIRMETS

EIS

FLIGHT
INSTRUMENTS

SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information)
are broadcast for potentially hazardous weather considered of extreme importance to all aircraft. A Convective
SIGMET is issued for hazardous convective weather. A localized SIGMET is a significant weather condition
occurring at a localized geographical position.

AUDIO PANEL
& CNS

AIRMET

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

SIGMET

Figure 6-22 SIGMET/AIRMET Data

Displaying SIGMETs and AIRMETs:
1) Select the Weather Data Link Page.

AFCS

2) Press the SIG/AIR Softkey.
3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the
icon.

ADDITIONAL
FEATURES

4) Press the ENT key. Figure 6-23 shows sample SIGMET text.

INDEX

APPENDICES

To display the SIGMET and AIRMET legend (Figure 6-24), press the LEGEND Softkey when SIGMETs and
AIRMETs are selected for display.

Figure 6-23 Sample SIGMET Text

294

Figure 6-24 SIGMET/AIRMET Legend

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SYSTEM
OVERVIEW

METARs and TAFs
NOTE: Atmospheric pressure as reported for METARs is given in hectopascals (hPa), except for in the United

FLIGHT
INSTRUMENTS

States, where it is reported in inches of mercury (in Hg). Temperatures are reported in Celsius.
Note: METAR information is only displayed within the installed aviation database service area.

EIS

METAR (METeorological Aerodrome Report) is the standard format for pre-flight weather briefings.
METARs are updated hourly and are considered current. METARs typically contain information about the
temperature, dewpoint, wind, precipitation, cloud cover, cloud heights, visibility, and barometric pressure.
They can also contain information on precipitation amounts, lightning, and other critical data. METARs are
shown as colored flags at airports that provide them.

AUDIO PANEL
& CNS

Instructions for
Viewing METAR and
TAF Text

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Selected Airport

AFCS

Figure 6-25 METAR Flags on the Weather Data Link Page
ADDITIONAL
FEATURES

TAF (Terminal Aerodrome Report) is the standard format for 24-hour weather forecasts. TAFs may contain
some METAR data, but generally cover a smaller area. It typically forecasts significant weather changes,
temporary changes, probable changes, and expected changes in weather conditions.

APPENDICES

METAR and TAF text are displayed on the Weather Information Page. METAR data is displayed first in a
decoded fashion, then as raw text. TAF information is displayed only in its raw form.
Displaying METAR and TAF text:
1) On the Weather Data Link Page, press the METAR Softkey.

INDEX

2) Press the RANGE Knob and pan to the desired airport.
3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text.

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SYSTEM
OVERVIEW

4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely
scrolled through before scrolling through the TAF text.

FLIGHT
INSTRUMENTS

Hazard Avoidance

5) Press the FMS Knob or the CLR Key to return to the Weather Data Link Page.
Or:

1) Select the Weather Information Page.

a) Turn the large FMS Knob to select the Waypoint Page Group.

b) Press the WX Softkey to select the Weather Information Page.

EIS

2) Press the FMS Knob to display the cursor.
3) Use the FMS Knob to enter the desired airport and press the ENT Key.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. Note that the METAR text must
be completely scrolled through before scrolling through the TAF text.

METAR Text for the
Selected Airport

HAZARD
AVOIDANCE

METAR Symbol

AFCS

TAF Text for the
Selected Airport

ADDITIONAL
FEATURES

Figure 6-26 METAR and TAF Text on the Weather Information Page

To display the METAR legend on the Weather Data Link Page (Figure 6-27), press the LEGEND Softkey when
METARs are selected for display.

INDEX

APPENDICES

The METAR flag color is determined by the information in the METAR text. A gray METAR flag is displayed
when the METAR text does not contain adequate information.

Figure 6-27 METAR Legend

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SYSTEM
OVERVIEW

Surface Analysis and City Forecast
Note: Surface Analysis and City Forecast data are displayed only within the installed Aviation Database

FLIGHT
INSTRUMENTS

service area.
Surface Analysis and City Forecast information is available for current and forecast weather conditions.
Forecasts are available for intervals of 12, 24, 36, and 48 hours.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Figure 6-28 Current Surface Analysis Data

Displaying Surface Analysis and City Forecast information:
AFCS

1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.

ADDITIONAL
FEATURES

3) Press the SFC Softkey.
4) Select the desired forecast time: CURRENT, 12 HR, 24 HR, 36 HR, or 48 HR. The SFC Softkey label changes
to reflect the forecast time selected.

APPENDICES

To display the Surface Analysis and City Forecast legend (Figure 2-29), press the LEGEND Softkey when
Surface Analysis and City Forecast are selected to be displayed.

INDEX

Figure 6-29 Surface Analysis Legend

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Hazard Avoidance
Freezing Levels

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Freezing Level data shows the color-coded contour lines for the altitude and location at which the first
isotherm is found (Figure 6-30). When no data is displayed for a given altitude, the data for that altitude has
not been received, or is out of date and has been removed from the display. New data appears at the next
update.

Figure 6-30 Freezing Level Data

Displaying Freezing Level information:
1) Select the Weather Data Link Page.

AFCS

2) Press the MORE WX Softkey.
3) Press the FRZ LVL Softkey.

APPENDICES

ADDITIONAL
FEATURES

To display the Freezing Level legend (Figure 6-31), press the LEGEND Softkey when Freezing Level data is
selected to be displayed.

INDEX

Figure 6-31 Freezing Level Legend

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SYSTEM
OVERVIEW

Winds Aloft
Winds Aloft data (Figure 6-32) shows the forecasted wind speed and direction at the surface and at selected
altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000 feet MSL.

FLIGHT
INSTRUMENTS

Displaying Winds Aloft data:
1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.
3) Press the WIND Softkey.

EIS

4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Press the NEXT or PREV Softkey to cycle
through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

Figure 6-32 Winds Aloft Data at 27,000 Feet

ADDITIONAL
FEATURES

To display the Winds Aloft legend (Figure 6-33), press the LEGEND Softkey when Winds Aloft is
selected for display.

APPENDICES

Figure 6-33 Winds Aloft Data with Legend
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance
Icing (CIP & SLD)

FLIGHT
INSTRUMENTS

Current Icing Product (CIP) data (Figure 6-34) shows a graphical view of the current icing environment.
Icing severity is displayed in four categories: light, moderate, severe, and extreme (not specific to aircraft type).
The CIP product is not a forecast, but a presentation of the current conditions at the time of the analysis.
Supercooled Large Droplet (SLD) icing conditions are characterized by the presence of relatively large,
super cooled water droplets indicative of freezing drizzle and freezing rain aloft. SLD threat areas are depicted
as magenta dots over the CIP colors.
Displaying Icing data:

EIS

1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.

AUDIO PANEL
& CNS

3) Press the ICNG Softkey.

FLIGHT
MANAGEMENT

4) Select the desired altitude level: 1,000 feet up to 30,000 feet. Press the NEXT or PREV Softkey to cycle through
the altitude softkeys. The ICNG Softkey label changes to reflect the altitude selected.

Supercooled
Large Droplets

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Light
Icing

Figure 6-34 Icing Data at 6,000 Feet

INDEX

APPENDICES

To display the Icing Potential legend (Figure 6-35), press the LEGEND Softkey when Icing is selected for
display.

Figure 6-35 Icing Potential Legend

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SYSTEM
OVERVIEW

Turbulence

FLIGHT
INSTRUMENTS

Turbulence data (Figure 6-36) identifies the potential for erratic movement of high-altitude air mass
associated winds. Turbulence is classified as light, moderate, severe or extreme, at altitudes between 21,000
and 45,000 feet.Turbulence data is intended to supplement AIRMETs and SIGMETs.
Displaying Turbulence data:
1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.
3) Press the TURB Softkey.

EIS

4) Select the desired altitude level: 21,000 feet up to 45,000 feet. Press the NEXT or PREV Softkey to cycle
through the altitude softkeys. The TURB Softkey label changes to reflect the altitude selected.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Severe
Turbulence

HAZARD
AVOIDANCE
AFCS

Figure 6-36 Turbulence Data at 21,000 Feet
ADDITIONAL
FEATURES

To display the Turbulence legend (Figure 6-37), press the LEGEND Softkey when Turbulence is selected
for display.

APPENDICES

Figure 6-37 Turbulence Legend

INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance
PIREPs and AIREPs

FLIGHT
INSTRUMENTS

Pilot Weather Reports (PIREPs) (Figure 6-38) provide timely weather information for a particular route of
flight. When significant weather conditions are reported or forecast, Air Traffic Control (ATC) facilities are
required to solicit PIREPs. A PIREP may contain unforecast adverse weather conditions, such as low in-flight
visibility, icing conditions, wind shear, and turbulence. PIREPs are issued as either Routine (UA) or Urgent
(UUA).
Another type of PIREP is an Air Report (AIREP). AIREPs are used almost exclusively by commerical airlines
at high altitudes.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Instructions for
Viewing PIREP
and AIREP Text

Routine
PIREP
Selected

AIREP

AFCS

HAZARD
AVOIDANCE

Urgent
PIREP

Figure 6-38 AIREPs and PIREPs on the Weather Data Link Page

ADDITIONAL
FEATURES

Displaying PIREP and AIREP text:
1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.
3) Press the AIREPS or PIREPS Softkey.

APPENDICES

4) Press the RANGE Knob and pan to the desired weather report. A gray circle will appear around the weather
report when it is selected.
5) Press the ENT Key. The Weather Information Page is shown with PIREP or AIREP text. The data is first displayed
in a decoded fashion, then as raw text.

INDEX

6) Use the FMS Knob or the ENT Key to scroll through the PIREP or AIREP text.
7) Press the FMS Knob or the CLR Key to return to the Weather Data Link Page.

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Hazard Avoidance
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

Decoded PIREP Text
EIS

Raw PIREP Text
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 6-39 PIREP Text on the Weather Data Link Page

HAZARD
AVOIDANCE

To display the PIREP or AIREP legend (Figure 6-40), press the LEGEND Softkey when PIREPs or AIREPs are
selected for display.
The PIREP color is determined by the type (routine or urgent).

AFCS
ADDITIONAL
FEATURES

Figure 6-40 AIREPs & PIREPs Legend

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance
County Warnings

FLIGHT
INSTRUMENTS

County data (Figure 6-41) provides specific public awareness and protection weather warnings from the
National Weather Service (NWS). This can include information on fires, tornadoes, severe thunderstorms,
flood conditions, and other natural disasters.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Additional
Information on
Flood Warning
Selected with
Map Pointer

HAZARD
AVOIDANCE

Flood Warning

Figure 6-41 County Flood Warning

Displaying County Warning information:
AFCS

1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.

ADDITIONAL
FEATURES

3) Press the COUNTY Softkey.

APPENDICES

To display the County Warnings legend (Figure 6-42), press the LEGEND Softkey when County Warnings
are selected to be displayed.

INDEX

Figure 6-42 County Warnings Legend

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Hazard Avoidance
SYSTEM
OVERVIEW

Cyclone
The Cyclone weather product (Figure 6-43) shows the current location of cyclones (hurricanes) and their
projected tracks.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

Cyclone

FLIGHT
MANAGEMENT

Figure 6-43 Cyclone Data Selected for Display

HAZARD
AVOIDANCE

Displaying cyclone (hurricane) track information:
1) Select the Weather Data Link Page.
2) Press the MORE WX Softkey.

AFCS

3) Press the CYCLONE Softkey.

To display the Cyclone legend (Figure 6-44), press the LEGEND Softkey when Cyclones are selected to be
displayed.

ADDITIONAL
FEATURES

Figure 6-44 Cyclone Legend

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance

6.2 WX-500 Stormscope

FLIGHT
INSTRUMENTS

NOTE: The Stormscope system is not intended for hazardous thunderstorm penetration. Weather information

on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 User’s Guide for a detailed
description of Stormscope operation.
Note: L-3 STORMSCOPE® WX-500 Lightning and GDL 69/69A XM® Satellite Weather Lightning are

EIS

mutually exclusive.
The following pages can display Stormscope data:

AUDIO PANEL
& CNS

• Stormscope Page
• Navigation Map

• AUX - Trip Planning Page
• Nearest Pages

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

To display Stormscope data on the Navigation Map, AUX - Trip Planning Page, or any of the Nearest Pages,
press the MAP Softkey, then press the STRMSCP Softkey. These pages can also display cell or strike data using the
yellow lightning strike symbology shown in Table 6-3.

Table 6-3 Lightning Age and Symbols

AFCS

Setting Up Stormscope on the Navigation Map
Setting up Stormscope options on the Navigation Map:
1) On the Navigation Map Page, press the MENU Key.
ADDITIONAL
FEATURES

2) With ‘Map Setup’ selected (Figure 6-45), press the ENT Key.
3) Turn the small FMS Knob to display the group selection window. Turn the small FMS Knob to select ‘Weather’
(Figure 6-46), and press the ENT Key.
4) Turn the large FMS Knob to highlight and move between the product selections.

APPENDICES

5) When an item is highlighted, turn the small FMS Knob to select the option.
6) Press the ENT Key.

INDEX

7) Press the FMS Knob to return to the Navigation Map Page.

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Hazard Avoidance
SYSTEM
OVERVIEW

The following options are available (Figure 6-46):
• STRMSCP LTNG – Turns the display of Stormscope data on or off.

FLIGHT
INSTRUMENTS

• STRMSCP MODE – Selects the CELL or STRIKE mode of lightning activity. Cell mode identifies clusters
or cells of electrical activity. Strike mode indicates the approximate location of lightning strikes.
• STRMSCP SMBL – Selects the range at which Stormscope data displays. Stormscope data is removed
when a map range greater than the STRMSCP SMBL value is selected.

EIS
AUDIO PANEL
& CNS

Figure 6-45 Page Menu

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 6-46 Map Setup Menu

Cell and Strike Mode on the Navigation Map

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INDEX

On the Navigation Map, cell mode identifies cells of lightning activity (Figure 6-40). Stormscope identifies
clusters of electrical activity that indicate cells. Strike mode indicates the approximate location of lightning
strikes.

307

SYSTEM
OVERVIEW

Hazard Avoidance
Selecting the ‘cell’ or ‘strike’ mode on the Navigation Map:
1) Press the MENU Key.

FLIGHT
INSTRUMENTS

2) With ‘Map Setup’ selected, press the ENT Key.
3) Select the ‘Weather’ group.
4) Press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’.
5) Turn the large FMS Knob to select ‘STRMSCP MODE’.

EIS

6) Turn the small FMS Knob to change between ‘CELL’ and ‘STRIKE’ options. When an item is selected, press the
ENT Key.

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

7) Press the FMS knob to return to the Navigation Map Page.

ADDITIONAL
FEATURES

Figure 6-47 Navigation Map Page with Stormscope
Lightning Data

APPENDICES

If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn
(Figure 6-4 1). This is to ensure that the strike and/or cell positions are depicted accurately in relation to the
nose of the aircraft.
Manually clearing Stormscope data on the Navigation Map:
1) Press the MENU Key.
2) Select ‘Clear Stormscope Lightning’.

INDEX

3) Press the ENT Key.

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Hazard Avoidance
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

Figure 6-48 Navigation Map Page Options Menu
EIS

Zoom Range on the Navigation Map
AUDIO PANEL
& CNS

Stormscope lightning data can be displayed up to 800 nm zoom range (in North up mode) on the Navigation
Map Page. However, in the track up mode at the 500 nm range, a portion of Stormscope lightning data
can be behind the aircraft and therefore not visible on the Navigation Map. Since the range for Stormscope
data is 400 nm diameter total (200 nm in front and 200 nm behind), the 500 nm range in North up mode
shows all the data.

FLIGHT
MANAGEMENT

At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The
presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right
corner (Figure 6-49).

HAZARD
AVOIDANCE

Figure 6-49 Lightning Display Range Annunciation
AFCS

Selecting a Stormscope range on the Navigation Map:
1) Press the MENU Key.

ADDITIONAL
FEATURES

2) Select ‘MAP SETUP’.
3) Select the ‘Weather’ group.
4) Press the ENT Key.

APPENDICES

5) Turn the large FMS Knob to select ‘STRMSCP SMBL’.
6) Turn the small FMS Knob to select the maximum display range.
7) Press the ENT Key.
8) Press the FMS Knob to return to the Navigation Map Page.

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INDEX

To change the display range on the Navigation Map Page, turn the RANGE Knob clockwise to zoom out or
counter-clockwise to zoom in.

309

SYSTEM
OVERVIEW

Hazard Avoidance

Selecting the Stormscope Page
Stormscope lightning data can be displayed at the ranges of 25 nm, 50 nm, 100 nm, and 200 nm.

FLIGHT
INSTRUMENTS

Adjusting the Stormscope Map Range:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Stormscope Page.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in.

AFCS

Figure 6-50 Stormscope Page

Changing between ‘cell’ and ‘strike’ mode on the Stormscope Page:

ADDITIONAL
FEATURES

1) Select the Stormscope Page.
2) Press the MODE Softkey. The CELL and STRIKE softkeys are displayed.
3) Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or
‘STRIKE’ is displayed in the mode box in the upper left corner of the Stormscope Page.

APPENDICES

4) Press the BACK Softkey to return to the main Stormscope page.

Changing the viewing mode between 360˚ and 120˚ on the Stormscope Page:
1) Select the Stormscope Page.

INDEX

2) Press the VIEW Softkey. The 360 and ARC softkeys are displayed. Press the 360 Softkey to display a 360˚
viewing area or press the ARC Softkey to display a 120˚ viewing area.
3) Press the BACK Softkey to return to the main Stormscope page.

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6.3 Terrain Proximity

FLIGHT
INSTRUMENTS

Warning: Do not use Terrain Proximity information for primary terrain avoidance. Terrain Proximity is

intended only to enhance situational awareness.
NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South.

EIS

G1000 Terrain Proximity is a terrain awareness system that does not comply with TSO-C151b certification
standards. It increases situational awareness and aids in reducing controlled flight into terrain (CFIT). Do not
confuse Terrain Proximity with Terrain Awareness and Warning System (TAWS). TAWS is more sophisticated
and robust, and it is TSO-C151b certified. Terrain Proximity does not provide warning annunciations or voice
alerts. It only provides color indications on map displays when terrain and obstacles are within a certain altitude
threshold from the aircraft. Although the terrain and obstacle color map displays are the same, TAWS uses more
sophisticated algorithms to assess aircraft distance from terrain and obstacles.

AUDIO PANEL
& CNS

Terrain Proximity requires the following components to operate properly:
• Valid 3-D GPS position

FLIGHT
MANAGEMENT

• Valid terrain/obstacle database

HAZARD
AVOIDANCE

Terrain Proximity displays altitudes of terrain and obstructions relative to the aircraft position and altitude with
reference to a database that may contain inaccuracies. Terrain and obstructions are shown only if they are in the
database. Terrain and obstacle information should be used as an aid to situational awareness. They should never
be used to navigate or maneuver around terrain.
Note that all obstructions may not be available in the terrain and obstacle database. No terrain and obstacle
information is shown without a valid 3-D GPS position.

AFCS

The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite
position. GPS altitude is then converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used
to determine terrain and obstacle proximity. GPS-MSL altitude accuracy is affected by satellite geometry, but is
not subject to variations in pressure and temperature that normally affect pressure altitude sensors. GPS-MSL
altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude
source.

ADDITIONAL
FEATURES
APPENDICES

Terrain and obstacle databases are referenced to MSL. Using the GPS position and altitude, the Terrain Proximity
feature portrays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the
aircraft. GPS position and GPS-MSL altitude are used to calculate and predict the aircraft’s flight path in relation
to the surrounding terrain and obstacles. In this way, the pilot can view predicted dangerous terrain and obstacle
conditions.

Displaying Terrain Proximity Data

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INDEX

The symbols and colors in Figure 6-51 and Table 6-4 are used to represent obstacles and aircraft altitude
when the Terrain Proximity Page is selected for display. Terrain Proximity uses black, yellow, and red to
represent terrain information relative to aircraft altitude. The color of each obstacle is associated with the
altitude of the aircraft.

311

SYSTEM
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Terrain Above Aircraft Altitude
Red terrain is above
or within 100 ft below
the aircraft altitude

Aircraft Altitude

FLIGHT
INSTRUMENTS

100 ft Threshold

1000 ft
Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude

EIS

Black terrain is more than 1000 ft below the aircraft altitude

Figure 6-51 Terrain Altitude/Color Correlation for Terrain Proximity
AUDIO PANEL
& CNS

Unlighted Obstacle
Lighted Obstacle
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL

Obstacle Location

FLIGHT
MANAGEMENT

Red obstacle is above or within 100 ft
below the aircraft altitude
Yellow obstacle is between 100 ft and
1000 ft below the aircraft altitude

HAZARD
AVOIDANCE

Table 6-4 Terrain Proximity Terrain/Obstacle Colors and Symbology

Terrain and obstacle information can be displayed on the following pages:
• PFD Inset Map

• Trip Planning Page

• Navigation Map Page

• Flight Plan Page

AFCS

• Terrain Proximity Page
Displaying terrain and obstacle information (maps other than the Terrain Proximity Page):
1) Press the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).
ADDITIONAL
FEATURES

2) Press the TERRAIN Softkey to display terrain and obstacle data.

When Terrain Proximity is selected on maps other than the Terrain Proximity Page, an icon to indicate the
feature is enabled for display and a legend for Terrain Proximity colors are shown (Figure 6-55).

APPENDICES

The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling
display of terrain and obstacles. The setup menu also controls the map range settings above which terrain and
obstacle data are decluttered from the display. If a map range larger than the map range setting is selected, the
data is removed from the map.

INDEX

Terrain data can be selected for display independently of obstacle data; however, obstacles recognized by
Terrain Proximity as yellow or red are shown when terrain is selected for display and the map range is within
the setting limit.

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Maps besides the Terrain Proximity Page use settings based on those selected for the Navigation Map Page.
The maximum display ranges for obstacles on each map are dependent on the range setting made for the
Navigation Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm,
the highest obstacle display range settings on the other applicable maps are also adjusted proportionally.

FLIGHT
INSTRUMENTS

Customizing terrain and obstacle display on the Navigation Map Page:
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-52).

EIS

4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-53).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-54).

AUDIO PANEL
& CNS

• TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown
• OBSTACLE DATA – Turns the display of obstacle data on or off and sets maximum range at which obstacles are shown
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.

FLIGHT
MANAGEMENT

8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

HAZARD
AVOIDANCE
AFCS

Figure 6-52 Navigation Map Page Menu

ADDITIONAL
FEATURES
APPENDICES

Figure 6-53 Navigation Map Page Setup Menu

Figure 6-54 Navigation Map Page Setup Menu, Map Group

INDEX

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Additional information about obstacles can be displayed by panning over the display on the map. The map
panning feature is enabled by pressing the RANGE Knob. The map range is adjusted by turning the RANGE
Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer.

FLIGHT
INSTRUMENTS

Additional Information
on Obstacle Selected
with Map Pointer
Yellow Terrain Area
(Between 100’ and
1000’ Below Aircraft
Altitude)

EIS

Red Terrain Area
(Above or Within
100’ Below Aircraft
Altitude)
Red Lighted
Obstacles
(Above or Within
100’ Below Aircraft
Altitude)

AUDIO PANEL
& CNS

Lighted Obstacle
Selected with Map
Pointer

FLIGHT
MANAGEMENT

Terrain Display
Enabled
Terrain Legend

HAZARD
AVOIDANCE

Figure 6-55 Terrain Information on the Navigation Map Page

Terrain Proximity Page

AFCS

The Terrain Proximity Page is specialized to show terrain and obstacle data in relation to the aircraft’s current
altitude, without clutter from the basemap. Aviation data (airports, VORs, and other NAVAIDs) can be displayed
for reference.

ADDITIONAL
FEATURES

Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available
relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map
range is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs).
Displaying the Terrain Proximity Page:
1) Turn the large FMS Knob to select the Map Page Group.

APPENDICES

2) Turn the small FMS Knob to select the Terrain Proximity Page.
3) To change the view,
a) Press the VIEW Softkey.
b) Press the 360 or ARC Softkey to select the desired view.
Or:
INDEX

a) Press the MENU Key.
b) Select ‘View 120º’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view.

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Showing/hiding aviation information on the Terrain Proximity Page:
1) Press the MENU Key.
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key.

FLIGHT
INSTRUMENTS

Map Orientation
Current Aircraft
GPS-derived MSL
Altitude

Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)

EIS

Yellow Terrain
(Between 100’ and
1000’ Below the
Aircraft Altitude)

Map Range Rings

AUDIO PANEL
& CNS

Black Terrain
(More than 1000’
Below the Aircraft
Altitude)

FLIGHT
MANAGEMENT

Terrain Legend

Figure 6-56 Terrain Proximity Page

HAZARD
AVOIDANCE
AFCS

Map Range Arcs

Yellow Terrain
(Between 100’ and
1000’ Below the
Aircraft Altitude)

ADDITIONAL
FEATURES

Black Terrain
(Terrain More than
1000’ Below the
Aircraft Altitude)

Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)

APPENDICES

Terrain Legend

Figure 6-57 Terrain Proximity Page (ARC View)
INDEX

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6.4 Terrain-SVS

FLIGHT
INSTRUMENTS

Warning: Do not use TERRAIN-SVS information for primary terrain avoidance. TERRAIN-SVS is intended

only to enhance situational awareness.
NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South.

EIS

NOTE: TERRAIN-SVS is standard when the Synthetic Vision System (SVS) option is installed. The TAWS

AUDIO PANEL
& CNS

G1000 TERRAIN-SVS is a terrain awareness system available with the Synthetic Vision System (SVS). SVS
functionality is offered as an optional enhancement. Optional Terrain Awareness and Warning System (TAWS)
or standard TERRAIN-SVS is integrated within SVS to provide visual and auditory alerts to indicate the presence
of threatening terrain relevant to the projected flight path. For detailed information regarding SVS, refer to the
Synthetic Vision System (SVS) section of the G1000 Pilot’s Guide.

FLIGHT
MANAGEMENT

option will take precedence over TERRAIN-SVS.

TERRAIN-SVS does not comply with TSO-C151b certification standards. It increases situational awareness and
aids in reducing controlled flight into terrain (CFIT). Do not confuse TERRAIN-SVS with Terrain Awareness and
Warning System (TAWS). TAWS is more sophisticated and robust, and it is TSO-C151b certified. Although the
terrain and obstacle color map displays are the same, TAWS uses more sophisticated algorithms to assess aircraft
distance from terrain and obstacles.

HAZARD
AVOIDANCE

TERRAIN-SVS does not provide the following:
• Premature Descent Alerting (PDA)
• Excessive Descent Rate (EDR)
• Negative Climb Rate (NCR)

AFCS

• Descent to 500 Feet Callout (DFC)
TERRAIN-SVS requires the following components to operate properly:
• Valid 3-D GPS position

ADDITIONAL
FEATURES

• Valid terrain/obstacle database

APPENDICES

TERRAIN-SVS displays altitudes of terrain and obstructions relative to the aircraft position and altitude with
reference to a database that may contain inaccuracies. Terrain and obstructions are shown only if they are in the
database. Terrain and obstacle information should be used as an aid to situational awareness. They should never
be used to navigate or maneuver around terrain.
Note that all obstructions may not be available in the terrain and obstacle database. No terrain and obstacle
information is shown without a valid 3-D GPS position.

INDEX

The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite
position. GPS altitude is then converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used
to determine terrain and obstacle proximity. GPS-MSL altitude accuracy is affected by satellite geometry, but is not
subject to variations in pressure and temperature that normally affect pressure altitude sensors. GPS-MSL altitude
does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source.

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OVERVIEW
FLIGHT
INSTRUMENTS

Terrain and obstacle databases are referenced to MSL. Using the GPS position and altitude, the TERRAIN-SVS
feature portrays a 3-D picture of the surrounding terrain and obstacles relative to the position and altitude of the
aircraft. GPS position and GPS-MSL altitude are used to calculate and predict the aircraft’s flight path in relation
to the surrounding terrain and obstacles. In this way, the pilot can view predicted dangerous terrain and obstacle
conditions.

Displaying TERRAIN-SVS Data

EIS

TERRAIN-SVS uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater
than 200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as
the aircraft altitude changes. The colors and symbols in Figure 6-51 and Table 6-5 are used to represent terrain,
obstacles, and potential impact points.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 6-58 Terrain Altitude/Color Correlation for TERRAIN-SVS
HAZARD
AVOIDANCE

Unlighted Obstacle
Lighted Obstacle
Potential
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Impact Points

Obstacle Location
WARNING: Red obstacle is above or within
100’ below current aircraft altitude

AFCS

CAUTION: Yellow obstacle is between 100’
and 1000’ below current aircraft altitude

ADDITIONAL
FEATURES

Table 6-5 TERRAIN-SVS Obstacle Colors and Symbology

TERRAIN-SVS information can be displayed on the following maps:
• Trip Planning Page

• Navigation Map Page

• Flight Plan Pages

APPENDICES

• PFD Inset Map
• TERRAIN-SVS Page

INDEX

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Displaying terrain and obstacle information (maps other than the TERRAIN-SVS Page):
1) Press the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).

FLIGHT
INSTRUMENTS

2) Press the TERRAIN Softkey to display terrain and obstacle data.

When TERRAIN-SVS is selected on maps other than the TERRAIN-SVS Page, an icon to indicate the feature
is enabled for display and a legend for TERRAIN-SVS terrain colors are shown (Figure 6-65).

EIS

AUDIO PANEL
& CNS

Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings
and cautions are issued are shown when terrain is selected for display and the map range is within the setting
limit.

FLIGHT
MANAGEMENT

Maps besides the TERRAIN-SVS Page use settings based on those selected for the Navigation Map Page. The
maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation
Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the
highest obstacle display range settings on the other applicable maps are also adjusted proportionally.
Customizing terrain and obstacle display on the Navigation Map Page:
1) Select the Navigation Map Page.
2) Press the MENU Key.

HAZARD
AVOIDANCE

3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-59).
4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-60).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-61).

AFCS

ADDITIONAL
FEATURES

6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.

INDEX

APPENDICES

8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

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SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS

Figure 6-59 Navigation Map Page Menu

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 6- 60 Navigation Map Page Setup Menu

Figure 6-61 Navigation Map Page Setup Menu, Map Group

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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OVERVIEW

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TERRAIN-SVS Page

FLIGHT
INSTRUMENTS

The TERRAIN-SVS Page is specialized to show terrain, obstacle, and potential impact point data in relation
to the aircraft’s current altitude, without clutter from the basemap. Aviation data (airports, VORs, and other
NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect,
the display automatically zooms in to the closest potential point of impact on the TERRAIN-SVS Page.
Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available
relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range
is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs).

EIS

Displaying the TERRAIN-SVS Page:
1) Turn the large FMS Knob to select the Map Page Group.

AUDIO PANEL
& CNS

2) Turn the small FMS Knob to select the TERRAIN-SVS Page.

Changing the TERRAIN-SVS Page view:
1) Press the VIEW Softkey.

FLIGHT
MANAGEMENT

2) Press the 360 or ARC Softkey to select the desired view.
Or:
1) Press the MENU Key.
2) Select ‘View 120º’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view

HAZARD
AVOIDANCE

Showing/hiding aviation information on the TERRAIN-SVS Page:
1) Press the MENU Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key.

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OVERVIEW
FLIGHT
INSTRUMENTS

Red Terrain
(Warning - Terrain
Above or Within
100’ Below the
Aircraft Altitude)

Yellow Terrain
(Caution - Terrain
Between 100’ and
1000’ Below the
Aircraft Altitude)

EIS

Black Terrain
(Terrain More than
1000’ Below the
Aircraft Altitude)

Map Range Rings
AUDIO PANEL
& CNS

Terrain Legend

FLIGHT
MANAGEMENT

Figure 6-62 TERRAIN-SVS Page

Yellow Terrain
(Caution - Terrain
Between 100’
and 1000’ Below
the Aircraft
Altitude)

HAZARD
AVOIDANCE

Red Terrain
(Warning - Terrain
Above or Within
100’ Below the
Aircraft Altitude)

AFCS

Black Terrain
(Terrain More than
1000’ Below the
Aircraft Altitude)

Map Range Arc

ADDITIONAL
FEATURES

Terrain Legend

APPENDICES

Figure 6-63 TERRAIN-SVS Page (ARC View)

INDEX

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TERRAIN-SVS Alerts

FLIGHT
INSTRUMENTS

Alerts are issued when flight conditions meet parameters that are set within TERRAIN-SVS software
algorithms. TERRAIN-SVS alerts typically employ a CAUTION or a WARNING alert severity level, or both.
When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table
6-6 shows TERRAIN-SVS alert types with corresponding annunciations and aural messages.

EIS

When an alert is issued, annunciations appear on the PFD and MFD. The TERRAIN-SVS Alert Annunciation
is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the
TERRAIN-SVS Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the
pop-up alert:
• Press the CLR Key (returns to the currently viewed page), or
• Press the ENT Key (accesses the TERRAIN-SVS Page)

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Alert Annunciation

Pop-up
Alert

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 6-64 TERRAIN-SVS Alert Annunciations

Terrain Display Enabled
Terrain Legend

INDEX

Alert Annunciation
Figure 6-65 Navigation Map Page
(After TERRAIN-SVS Pop-up Alert Acknowledgment)

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Alert Type

MFD
Pop-Up Alert

Aural Message
“Warning; Terrain, Terrain”

Imminent Terrain Impact Warning (ITI)

“Warning; Terrain, Terrain”

Reduced Required Obstacle Clearance
Warning (ROC)

“Warning; Obstacle, Obstacle”

Imminent Obstacle Impact Warning (IOI)

“Warning; Obstacle, Obstacle”

Imminent Terrain Impact Caution (ITI)

“Caution; Terrain, Terrain”

Reduced Required Obstacle Clearance
Caution (ROC)

“Caution; Obstacle, Obstacle”

Imminent Obstacle Impact Caution (IOI)

“Caution; Obstacle, Obstacle”

FLIGHT
MANAGEMENT

“Caution; Terrain, Terrain”

AUDIO PANEL
& CNS

Reduced Required Terrain Clearance
Caution (RTC)

EIS

Reduced Required Terrain Clearance
Warning (RTC)

FLIGHT
INSTRUMENTS

PFD/MFD
Alert
Annunciation

Table 6-6 TERRAIN-SVS Alerts Summary

HAZARD
AVOIDANCE

Forward Looking Terrain Avoidance

AFCS

Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC)
alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum
clearance values in Figure 6-66. When an RTC alert is issued, a potential impact point is displayed on the
TERRAIN-SVS Page.

ADDITIONAL
FEATURES

Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the
aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts
are accompanied by a potential impact point displayed on the TERRAIN-SVS Page. The alert is annunciated
when the projected vertical flight path is calculated to come within minimum clearance altitudes in Figure
6-66.

APPENDICES
INDEX

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Required Terrain Clearance
RTC Level (FT)

RTC Descending (FT)

800

EIS

Required
Terrain
Clearance
(FT)
Required
Terrain Clearance
(FT)

FLIGHT
INSTRUMENTS

700

600

500

400

300

200

AUDIO PANEL
& CNS

100

0
0

Distance From Runway (NM)
Distance
From Runway (NM)

FLIGHT
MANAGEMENT

Figure 6-66 FLTA Alert Minimum Terrain and Obstacle Clearance Values

FLTA alerts are automatically inhibited when the aircraft is less than 200 feet above the destination runway
elevation while within 0.5 nm of the approach runway or the aircraft is between runway ends

HAZARD
AVOIDANCE

PDA and FLTA aural and visual alerts can be manually inhibited. Discretion should be used when inhibiting
TERRAIN-SVS and the system should be enabled when appropriate. When TERRAIN-SVS is inhibited, the
alert annunciation ‘TER INH’ is shown on the PFD and MFD (Figure 6-67).

AFCS

Figure 6-67 TERRAIN-SVS Alerting Disabled
(TERRAIN-SVS Inhibited) Annunciation

Inhibiting/enabling TERRAIN-SVS alerting:

ADDITIONAL
FEATURES

1) Select the TERRAIN-SVS Page.
2) Press the INHIBIT Softkey to inhibit or enable TERRAIN-SVS (choice dependent on current state).

Or:
a) Press the MENU Key.

APPENDICES

b) Select ‘Inhibit TERRAIN-SVS’ or ‘Enable TERRAIN-SVS’ (choice dependent on current state) and press the ENT
Key.

INDEX

If TERRAIN-SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS
approach, a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft
altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments
Section for details.

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SYSTEM
OVERVIEW

System Status
During power-up, TERRAIN-SVS conducts a self-test of its aural and visual annunciations. An aural alert is
issued at test completion.
PFD/MFD Alert
Annunciation

Aural Message
None

System Test in Progress
System Test Pass

FLIGHT
INSTRUMENTS

Alert Type

None

“Terrain System Test OK”
“Terrain System Failure”

Terrain System Test Fail

EIS

Table 6-7 TERRAIN-SVS System Test Status Annunciations
AUDIO PANEL
& CNS

TERRAIN-SVS continually monitors several system-critical items such as database validity, hardware status,
and GPS status. If the terrain/obstacle database is not available, the aural message “Terrain System Failure”
is generated along with the ‘TER FAIL’ alert annunciation.

Alert Type
No GPS position
Excessively degraded GPS signal
GPS signal re-established

Aural Message
HAZARD
AVOIDANCE

PFD/MFD Alert
Annunciation

FLIGHT
MANAGEMENT

TERRAIN-SVS requires a 3-D GPS navigation solution along with specific vertical accuracy minimums.
Should the navigation solution become degraded or if the aircraft is out of the database coverage area, the
annunciation ‘TER N/A’ is generated in the annunciation window and on the TERRAIN-SVS Page. The aural
message “Terrain System Not Available” is generated. When the GPS signal is re-established and the aircraft
is within the database coverage area, the aural message “Terrain System Available” is generated.

“Terrain System Not Available”
None

“Terrain System Available”
AFCS

Table 6-8 TERRAIN-SVS Status Annunciations

ADDITIONAL
FEATURES
APPENDICES
INDEX

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6.5 Terrain Awareness & Warning System (TAWS)

FLIGHT
INSTRUMENTS

Warning: Do not use TAWS information for primary terrain avoidance. TAWS is intended only to enhance

situational awareness.
NOTE: The data contained in the TAWS databases comes from government agencies. Garmin accurately

processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data.

AUDIO PANEL
& CNS

EIS

TAWS (Terrain Awareness and Warning System) is an optional feature to increase situational awareness and aid
in reducing controlled flight into terrain (CFIT). TAWS provides visual and aural annunciations when terrain and
obstacles are within the given altitude threshold from the aircraft. The displayed alerts and warnings are advisory
in nature only.
TAWS satisfies TSO-C151b Class B requirements for certification. Class B TAWS is required for all Part 91
aircraft operations with six or more passenger seats and for Part 135 turbine aircraft operations with six to nine
passenger seats (FAR Parts 91.223, 135.154).

FLIGHT
MANAGEMENT

TAWS requires the following to operate properly:
• A valid terrain/obstacle/airport terrain database
• A valid 3-D GPS position solution

HAZARD
AVOIDANCE

TAWS uses terrain and obstacle information supplied by government sources. Terrain information is based on
terrain elevation information in a database that may contain inaccuracies. Individual obstructions may be shown
if available in the database. The data undergoes verification by Garmin to confirm accuracy of the content, per
TSO-C151b. However, the displayed information should never be understood as being all-inclusive and data
may be inaccurate.

ADDITIONAL
FEATURES

AFCS

TAWS uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS
altitude is derived from satellite measurements. GPS altitude is converted to a mean sea level (MSL)-based altitude
(GPS-MSL altitude) and is used to determine TAWS alerts. GPS-MSL altitude accuracy is affected by factors such
as satellite geometry, but it is not subject to variations in pressure and temperature that normally affect pressure
altitude devices. GPS-MSL altitude does not require local altimeter settings to determine MSL altitude. Therefore,
GPS altitude provides a highly accurate and reliable MSL altitude source to calculate terrain and obstacle alerts.

APPENDICES

The terrain and obstacle databases used by TAWS are referenced to mean sea level (MSL). Using the GPS
position and GPS-MSL altitude, TAWS displays a 2-D (or 3-D with SVS) picture of the surrounding terrain and
obstacles relative to the position and altitude of the aircraft. Furthermore, the GPS position and GPS-MSL altitude
are used to calculate and “predict” the aircraft’s flight path in relation to the surrounding terrain and obstacles. In
this manner, TAWS can provide advanced alerts of predicted dangerous terrain conditions.

INDEX

Baro-corrected altitude (or indicated altitude) is derived by adjusting the altimeter setting for local atmospheric
conditions. The most accurate baro-corrected altitude can be achieved by frequently updating the altimeter setting
to the nearest reporting station along the flight path. However, because actual atmosphere conditions seldom
match the standard conditions defined by the International Standard Atmosphere (ISA) model (where pressure,
temperature, and lapse rates have fixed values), it is common for the baro-corrected altitude (as read from the
altimeter) to differ from the GPS-MSL altitude. This variation results in the aircraft’s true altitude differing from
the baro-corrected altitude.

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SYSTEM
OVERVIEW

Displaying TAWS Data

FLIGHT
INSTRUMENTS

TAWS uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater than 200
feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the aircraft
altitude changes. The colors and symbols in Figure 6-60 and Table 6-9 are used to represent terrain, obstacles,
and potential impact points.

EIS
AUDIO PANEL
& CNS

Figure 6-68 Terrain Altitude/Color Correlation for TAWS

FLIGHT
MANAGEMENT

Unlighted Obstacle
Lighted Obstacle
Potential
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Impact Points

Obstacle Location

HAZARD
AVOIDANCE

WARNING: Red obstacle is above or within
100’ below current aircraft altitude
CAUTION: Yellow obstacle is between 100’
and 1000’ below current aircraft altitude
Table 6-9 TAWS Obstacle Colors and Symbology

AFCS

TAWS information can be displayed on the following maps:
• Trip Planning Page

• Navigation Map Page

• Flight Plan Pages

ADDITIONAL
FEATURES

• PFD Inset Map
• TAWS-B Page

Displaying terrain and obstacle information (maps other than the TAWS Page):

APPENDICES

1) Press the MAP Softkey (for the PFD Inset Map, select the INSET Softkey).
2) Press the TERRAIN Softkey to display terrain and obstacle data.

When TAWS is selected on maps other than the TAWS-B Page, an icon to indicate the feature is enabled for
display and a legend for TAWS terrain colors are shown (Figure 6-75).

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327

SYSTEM
OVERVIEW

Hazard Avoidance
Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings
and cautions are issued are shown when terrain is selected for display and the map range is within the setting
limit.

FLIGHT
INSTRUMENTS

Maps besides the TAWS-B Page use settings based on those selected for the Navigation Map Page. The
maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation
Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the highest
obstacle display range settings on the other applicable maps are also adjusted proportionally.
Customizing terrain and obstacle display on the Navigation Map Page:

EIS

1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-69).

AUDIO PANEL
& CNS

4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-70).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-71).
• TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown

FLIGHT
MANAGEMENT

• OBSTACLE DATA – Turns the display of obstacle data on or off and sets maximum range at which obstacles are shown
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.

AFCS

HAZARD
AVOIDANCE

8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 6-69 Navigation Map Page Menu

Figure 6-70 Navigation Map Page Setup Menu

328

Figure 6-71 Navigation Map Page Setup Menu, Map Group

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SYSTEM
OVERVIEW

TAWS-B Page

FLIGHT
INSTRUMENTS

The TAWS-B Page is specialized to show terrain, obstacle, and potential impact point data in relation to
the aircraft’s current altitude, without clutter from the basemap. Aviation data (airports, VORs, and other
NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect,
the display automatically zooms in to the closest potential point of impact on the TAWS-B Page.
Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available
relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map
range is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs).

EIS

Displaying the TAWS-B Page:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the TAWS Page.

AUDIO PANEL
& CNS

Changing the TAWS-B Page view:
1) Press the VIEW Softkey.
2) Press the 360 or ARC Softkey to select the desired view.

FLIGHT
MANAGEMENT

Or:
1) Press the MENU Key.
2) Select ‘View 120º’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view

HAZARD
AVOIDANCE

Showing/hiding aviation information on the TAWS-B Page:
1) Press the MENU Key.
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance

Red Terrain
(Warning - Terrain
Above or Within
100’ Below the
Aircraft Altitude)

EIS

FLIGHT
INSTRUMENTS

Yellow Terrain
(Caution - Terrain
Between 100’ and
1000’ Below the
Aircraft Altitude)

Black Terrain
(Terrain More than
1000’ Below the
Aircraft Altitude)

AUDIO PANEL
& CNS

Map Range Rings

Terrain Legend

FLIGHT
MANAGEMENT

Annunciation
Window
Figure 6-72 TAWS-B Page

HAZARD
AVOIDANCE

Yellow Terrain
(Caution - Terrain
Between 100’
and 1000’ Below
the Aircraft
Altitude)

Red Terrain
(Warning - Terrain
Above or Within
100’ Below the
Aircraft Altitude)
Black Terrain
(Terrain More than
1000’ Below the
Aircraft Altitude)

ADDITIONAL
FEATURES

AFCS

Map Range Arc

Terrain Legend

APPENDICES

Annunciation
Window

INDEX

Figure 6-73 TAWS-B Page (ARC View)

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SYSTEM
OVERVIEW

TAWS Alerts

FLIGHT
INSTRUMENTS

Alerts are issued when flight conditions meet parameters that are set within TAWS software algorithms.
TAWS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued,
visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-10 shows TAWS alert
types with corresponding annunciations and aural messages.
When an alert is issued, annunciations appear on the PFD and MFD. The TAWS Alert Annunciation is shown
to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TAWS-B Page is
not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert:

EIS

• Press the CLR Key (returns to the currently viewed page), or
• Press the ENT Key (accesses the TAWS-B Page)
Alert Annunciation

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Pop-up
Alert

Figure 6-74 TAWS Alert Annunciations

AFCS
ADDITIONAL
FEATURES
APPENDICES

Terrain Display Enabled
Terrain Legend
Alert Annunciation

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INDEX

Figure 6-75 Navigation Map Page
(After TAWS Pop-up Alert Acknowledgment)

331

SYSTEM
OVERVIEW

Hazard Avoidance
PFD/MFD Alert
Annunciation

Alert Type

MFD Pop-Up Alert

Aural Message

FLIGHT
INSTRUMENTS

Excessive Descent Rate Warning
(EDR)

“Pull Up”

Reduced Required Terrain
Clearance Warning (RTC)

EIS

Imminent Terrain Impact
Warning (ITI)

AUDIO PANEL
& CNS

Reduced Required Obstacle
Clearance Warning (ROC)

FLIGHT
MANAGEMENT

Imminent Obstacle Impact
Warning (IOI)
Reduced Required Terrain
Clearance Caution (RTC)

HAZARD
AVOIDANCE
AFCS

* “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”*
or
“Obstacle, Obstacle; Pull Up, Pull Up”
*

“Terrain Ahead; Terrain Ahead”*
or
“Caution, Terrain; Caution, Terrain”

“Obstacle Ahead; Obstacle Ahead”*
or
“Caution, Obstacle; Caution, Obstacle”

Imminent Obstacle Impact
Caution (IOI)

Premature Descent Alert
Caution (PDA)
Altitude Callout “500”
Excessive Descent Rate Caution
(EDR)

ADDITIONAL
FEATURES

* “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”*
or
“Obstacle, Obstacle; Pull Up, Pull Up”

Reduced Required Obstacle
Clearance Caution (ROC)

APPENDICES

Terrain Ahead, Pull Up; Terrain Ahead, Pull Up’*
or
“Terrain, Terrain; Pull Up, Pull Up”

Imminent Terrain Impact Caution
(ITI)

Negative Climb Rate Caution
(NCR)

* “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”*
or
“Terrain, Terrain; Pull Up, Pull Up”

“Too Low, Terrain”
None

None

“Five-Hundred”
“Sink Rate”
*

“Don’t Sink”*
or
“Too Low, Terrain”

* Alerts with multiple messages are configurable at installation and are installation-dependent. Alerts for the default
configuration are indicated with asterisks.

INDEX

Table 6-10 TAWS Alerts Summary

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SYSTEM
OVERVIEW

Excessive Descent Rate Alert

FLIGHT
INSTRUMENTS

The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the
aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-76 shows the
parameters for the alert as defined by TSO-C151b.
6000
5500
5000

4000

NK
: “SI

ion

Caut

3500

”

RATE

EIS

Height Above Terrain (Feet)

4500

3000

AUDIO PANEL
& CNS

2500
2000

Warning: “PULL UP”

1500
1000

12000

11000

10000

9000

8000

7000

6000

5000

4000

3000

2000

1000

Descent Rate (FPM)

FLIGHT
MANAGEMENT

500

Figure 6-76 Excessive Descent Rate Alert Criteria

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance
Forward Looking Terrain Avoidance

FLIGHT
INSTRUMENTS

Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC)
alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum
clearance values in Figure 6-77. When an RTC alert is issued, a potential impact point is displayed on the
TAWS-B Page.

EIS

Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the
aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts are
accompanied by a potential impact point displayed on the TAWS-B Page. The alert is annunciated when the
projected vertical flight path is calculated to come within minimum clearance altitudes in Figure 6-77.
Required Terrain Clearance
RTC Level (FT)

RTC Descending (FT)

AUDIO PANEL
& CNS

800

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Required
Terrain
Clearance
(FT)
Required
Terrain Clearance
(FT)

700

600

500

400

300

200

100

0
0

Distance From Runway (NM)
Distance
From Runway (NM)

AFCS

Figure 6-77 FLTA Alert Minimum Terrain and Obstacle Clearance Values

INDEX

APPENDICES

ADDITIONAL
FEATURES

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SYSTEM
OVERVIEW

Premature Descent Alerting
A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly
below the normal approach path to a runway (Figure 6-78).

FLIGHT
INSTRUMENTS

PDA alerting begins when the aircraft is below 700 feet AGL within 15 nm of the destination airport and
ends when the aircraft is 0.5 nm from the runway threshold.
800

600

EIS

500

400

AUDIO PANEL
& CNS

Height Above Destination (Feet)

700

300

PDA Alerting Area

200

100

FLIGHT
MANAGEMENT

Distance to Destination (NM)
Figure 6-78 PDA Alerting Threshold

HAZARD
AVOIDANCE

PDA and FLTA aural and visual alerts can be manually inhibited. Discretion should be used when inhibiting
TAWS and the system should be enabled when appropriate. When TAWS is inhibited, the alert annunciation
‘TAWS INH’ is shown on the PFD and MFD (Figure 6-79).

AFCS

Figure 6-79 TAWS Alerting Disabled
(TAWS Inhibited) Annunciation

Inhibiting/enabling TAWS alerting:
ADDITIONAL
FEATURES

1) Select the TAWS-B Page.
2) Press the INHIBIT Softkey to inhibit or enable TAWS (choice dependent on current state).
Or:

APPENDICES

a) Press the MENU Key.
b) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key.

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INDEX

If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach,
a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft altitude is at
least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section
for details.

335

SYSTEM
OVERVIEW

Hazard Avoidance
Five-Hundred Aural Alert

FLIGHT
INSTRUMENTS

The purpose of the aural alert message “Five-hundred” is to provide an advisory alert that the aircraft is 500
feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Five-hundred” is
generated. There are no display annunciations or pop-up alerts that accompany the aural message.

Negative Climb Rate After Takeoff Alert (NCR)

EIS

The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”)
provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff.
The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain
alert on the display. NCR alerting is only active when departing from an airport and when the following
conditions are met:

AUDIO PANEL
& CNS

• Height above the terrain is less than 700 feet
• Distance from the departure airport is 2 nm or less
• Heading change from the departure heading is less than 110 degrees

FLIGHT
MANAGEMENT

Figures 6-80 and 6-81 show the NCR alerting parameters as defined by TSO-C151b.
1000

HAZARD
AVOIDANCE

Height Above Terrain (Feet)

900
800
700
600

“DON’T SINK”
or
“TOO LOW, TERRAIN”

500
400
300

AFCS

200
100
0
0

100

120

140

ADDITIONAL
FEATURES

Altitude Loss (Feet)

INDEX

APPENDICES

Figure 6-80 Negative Climb Rate (NCR) Altitude Loss

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Hazard Avoidance
SYSTEM
OVERVIEW

1000

800
700

FLIGHT
INSTRUMENTS

Height Above Terrain (Feet)

900

600

“DON’T SINK”
or
“TOO LOW, TERRAIN”

500
400
300

EIS

200
100
0
0

500

1000

1500

2000

2500

3000

3500

4000

4500

5000

5500

6000

6500

7000

AUDIO PANEL
& CNS

Sink Rate (FPM)
Figure 6-81 Negative Climb Rate (NCR) Sink Rate

FLIGHT
MANAGEMENT

System Status
During power-up, TAWS conducts a self-test of its aural and visual annunciations. The system test can also be
manually initiated. An aural alert is issued at test completion. TAWS System Testing is disabled when ground
speed exceeds 30 knots.

HAZARD
AVOIDANCE

PFD/MFD Alert
Annunciation

Alert Type

Aural Message
None

System Test in Progress
System Test Pass

None

“TAWS System Test OK”
“TAWS System Failure”

TAWS System Test Fail

AFCS

Table 6-11 TAWS System Test Status Annunciations

Manually testing the TAWS System:
ADDITIONAL
FEATURES

1) Select the TAWS-B Page.
2) Press the MENU Key (Figure 6-82).
3) Select ‘Test TAWS’ and press the ENT Key to confirm the selection.

APPENDICES
INDEX

Figure 6-82 TAWS-B Page Menu

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SYSTEM
OVERVIEW

Hazard Avoidance
TAWS continually monitors several system-critical items such as database validity, hardware status, and GPS
status. If the terrain/obstacle database is not available, the aural message “TAWS System Failure” is generated
along with the ‘TAWS FAIL’ alert annunciation.

FLIGHT
INSTRUMENTS

TAWS requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the
navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation
‘TAWS N/A’ is generated in the annunciation window and on the TAWS Page. The aural message “TAWS Not
Available” is generated. When the GPS signal is re-established and the aircraft is within the database coverage
area, the aural message “TAWS Available” is generated.

EIS

Alert Type

PFD/MFD Alert
Annunciation

AUDIO PANEL
& CNS

No GPS position
Excessively degraded GPS signal
GPS signal re-established

Aural Message
“TAWS Not Available”

None

“TAWS Available”

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Table 6-12 TAWS Status Annunciations

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Hazard Avoidance
SYSTEM
OVERVIEW

6.6 Traffic Information Service (TIS)

FLIGHT
INSTRUMENTS

WARNING: The Traffic Information Service (TIS) is intended for advisory use only. TIS is intended to help the
pilot locate traffic visually. It is the responsibility of the pilot to see and maneuver to avoid traffic.
NOTE: TIS is available only when the aircraft is within the service volume of a TIS-capable terminal radar

EIS

site. Aircraft without an operating transponder are invisible to both Traffic Advisory Systems (TAS) and TIS.
Aircraft without altitude reporting capability are shown without altitude separation data or climb descent
indication.
NOTE: TIS is disabled if a Traffic Advisory System (TAS) is installed.

AUDIO PANEL
& CNS

TIS Symbol

FLIGHT
MANAGEMENT

Traffic Information Service (TIS) is designed to help in detection and avoidance of other aircraft. TIS uses the
Mode S transponder for the traffic data link. TIS receives traffic information from ground stations, and is updated
every 5 seconds. The G1000 displays up to eight traffic targets within a 7.5-nm radius, from 3000 feet below to
3500 feet above the requesting aircraft. Traffic is displayed according to TCAS symbology using three different
symbols (Table 6-13).
Description
Non-Threat Traffic

HAZARD
AVOIDANCE

Traffic Advisory (TA)
Traffic Advisory Off Scale

AFCS

Table 6-13 TIS Traffic Symbols

ADDITIONAL
FEATURES

Proximity Advisories (PAs) are defined as traffic within the 5.0-nm range, within ±1200 feet of altitude separation.
They are not Traffic Advisories (TA), which alert the crew to intruding aircraft. When traffic meets the advisory
criteria for the TA, a solid yellow circle symbol is generated. A TA which is detected but is outside the range of
the map on which traffic is displayed are indicated with a message in the lower left corner of the map.

APPENDICES

TIS also provides a vector line showing the direction in which the traffic is moving, to the nearest 45°. Traffic
information for which TIS is unable to determine the bearing (non-bearing traffic) is displayed in the center of
the Traffic Map Page (Figure 6-87) or in a banner at the lower left corner of maps other than the Traffic Map Page
on which traffic can be displayed.

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INDEX

The altitude difference between the requesting aircraft and other intruder aircraft is displayed above/below the
traffic symbol in hundreds of feet. If the other aircraft is above the requesting aircraft, the altitude separation
appears above the traffic symbol; if below, the altitude separation appears below. Altitude trend is displayed as
an up/down arrow (for speeds greater than 500 fpm in either direction) to the right of the target symbol. Traffic
symbols for aircraft without altitude reporting capability appear without altitude separation or climb/descent
information.

339

SYSTEM
OVERVIEW

Hazard Avoidance

Displaying TRAFFIC Data

FLIGHT
INSTRUMENTS

Traffic information can be displayed on the following maps (when TIS is operating):
• PFD Inset Map

• Trip Planning Page

• Navigation Map Page

• Nearest Pages

• Traffic Map Page

• Active Flight Plan Page

EIS

Displaying traffic information (maps other than the Traffic Map Page):
1) Press the MAP Softkey.
2) Press the TRAFFIC Softkey to display traffic data.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

When traffic is selected on maps other than the Traffic Map Page, an icon is shown to indicate the feature is
enabled for display.

AFCS

HAZARD
AVOIDANCE

Traffic Advisory

Traffic Display
Enabled

ADDITIONAL
FEATURES

Traffic Status
Banner

INDEX

APPENDICES

Figure 6-83 TIS Traffic on the Navigation Map Page

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Hazard Avoidance
SYSTEM
OVERVIEW

Displaying traffic information (PFD Inset Map):
1) Press the INSET Softkey.
2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1).

FLIGHT
INSTRUMENTS

3) Press the softkey again to display the traffic-only inset (TRFC-2).
4) Press the softkey again to remove traffic data.

EIS

The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling
display of traffic. The setup menu also controls the map range settings above which traffic data (symbols
and labels) are decluttered from the display. If a map range larger than the map range setting is selected, the
data is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the
Navigation Map Page.
Customizing traffic display on the Navigation Map Page:

AUDIO PANEL
& CNS

1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-84).

FLIGHT
MANAGEMENT

4) Turn the small FMS Knob to select the ‘Traffic’ Group and press the ENT Key (Figure 6-85).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-86).
• TRAFFIC – Turns the display of traffic data on or off

- All Traffic - Displays all traffic

- TA/PA - Displays Traffic Alerts and Proximity Advisories

- TA ONLY - Displays Traffic Alerts only

HAZARD
AVOIDANCE

• TRAFFIC MODE – Selects the traffic mode for display; select from:

• TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown
AFCS

• TRAFFIC LBL – Selects the maximum range at which traffic labels are shown (with the option to turn off)
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.).

ADDITIONAL
FEATURES

7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.

APPENDICES
INDEX

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341

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Hazard Avoidance

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Figure 6-84 Navigation Map Page Menu

Figure 6-85 Navigation Map Page Setup Menu

Figure 6-86 Navigation Map Page Setup Menu, Traffic Group

HAZARD
AVOIDANCE

Traffic Map Page
The Traffic Map Page is specialized to show surrounding TIS traffic data in relation to the aircraft’s current
position and altitude, without clutter from the basemap. Aircraft orientation on this map is always heading up
unless there is no valid heading. Map range is adjustable with the RANGE Knob from 2 to 12 nm, as indicated
by the map range rings.

AFCS

The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the
ground, TIS automatically enters Standby Mode. Once the aircraft is airborne, TIS switches from Standby to
Operating Mode and the G1000 begins to display traffic information. Refer to the System Status discussion for
more information.

ADDITIONAL
FEATURES

Displaying traffic on the Traffic Map Page:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.

APPENDICES

3) Confirm TIS is in Operating Mode:
Press the OPERATE Softkey to begin displaying traffic.
Or:
a) Press the MENU Key.

INDEX

b) Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the ENT Key.

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SYSTEM
OVERVIEW

Traffic Mode Annunciation
“TIS Not Available”
Voice Alert Status

FLIGHT
INSTRUMENTS

“Non-Bearing” Traffic
(System Unable to
Determine Bearing)
Distance is 8.0 nm,
1100’ Above,
Descending

AUDIO PANEL
& CNS

Traffic Advisory
400’ Below,
Climbing

EIS

Range
Marking
Rings

Non-Threat
Traffic

Figure 6-87 Traffic Map Page

FLIGHT
MANAGEMENT

Traffic Status
Banner

Select
to Mute
“TIS Not
Available”
Voice Alert

HAZARD
AVOIDANCE

TIS Alerts
When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur:
• A single “Traffic” voice alert is generated.

AFCS

• A ‘TRAFFIC’ Annunciation appears to the top left of the Attitude Indicator on the PFD, flashing for 5 seconds
and remaining displayed until no TAs are detected in the area.
• The PFD Inset Map is automatically displayed with traffic.

ADDITIONAL
FEATURES

To reduce the number of nuisance alerts due to proximate aircraft, the “Traffic” voice alert is generated only
when the number of TAs increases. For example, when the first TA is displayed, a voice and visual annunciation
are generated. As long as a single TA remains on the display, no additional voice alerts are generated. If a second
TA appears on the display or if the number of TAs initially decreases and then subsequently increases, another
voice alert is generated.

APPENDICES
INDEX

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FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Hazard Avoidance

AUDIO PANEL
& CNS

EIS

Inset Map
Displays When
TA is Detected

Figure 6-88 Traffic Annunciation (PFD)

A “TIS Not Available” (TNA) voice alert is generated when the TIS service becomes unavailable or is out of
range. TIS may be unavailable in the radar coverage area due to the following:

FLIGHT
MANAGEMENT

• Radar site TIS Mode S sensor is not operational or is out of service
• Traffic or requesting aircraft is beyond the maximum range of the TIS-capable Mode S radar site.
• Traffic or requesting aircraft is above the radar site in the cone of silence and out of range of an adjacent site.

HAZARD
AVOIDANCE

• Traffic or requesting aircraft is below radar coverage. In flat terrain, the coverage extends from about 3000
feet upward at 55 miles. Terrain and obstacles around the radar site can further decrease radar coverage in all
directions.
• Traffic does not have an operating transponder.

AFCS

The “TIS Not Available” (TNA) voice alert can be manually muted to reduce nuisance alerting. TNA muting
status is shown in the upper left corner of the Traffic Map Page.
Muting the “TIS Not Available” voice alert:
ADDITIONAL
FEATURES

1) Select the Traffic Map Page.
2) Press the TNA MUTE Softkey. The status is displayed in the upper left corner of the Traffic Map Page.

Or:
a) Press the MENU Key.

INDEX

APPENDICES

b) Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off) and press the ENT Key.

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SYSTEM
OVERVIEW

System Status

Traffic Map Page
Annunciation
NO DATA

FAILED

Description
Data is not being received from the transponder*
Data is being received from the transponder, but
a failure is detected in the data stream*

EIS

DATA FAILED

FLIGHT
INSTRUMENTS

The G1000 performs an automatic test of TIS during power-up. If TIS passes the test, TIS enters Standby
Mode (on the ground) or Operating Mode (in the air). If TIS fails the power up test, an annunciation is shown
in the center of the Traffic Map Page.

The transponder has failed*
TIS is unavailable or out of range

AUDIO PANEL
& CNS

UNAVAILABLE

* Contact a service center or Garmin dealer for corrective action
Table 6-14 TIS Failure Annunciations

FLIGHT
MANAGEMENT

System Test has Failed

HAZARD
AVOIDANCE

Data Not Received
from Transponder
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 6-89 TIS Power-up Test Failure

INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the
ground, TIS automatically enters Standby Mode. If traffic is selected for display on another map while Standby
Mode is selected, the traffic display enabled icon is crossed out (also the case whenever TIS has failed). Once
the aircraft is airborne, TIS switches to Operating Mode and traffic information is displayed. The mode can be
changed manually using softkeys or the page menu.
Mode

Traffic Mode Annunciation
(Traffic Map Page)

TIS Operating

OPERATING

TIS Standby

STANDBY
(also shown in white in center of page)

TIS Failed*

FAIL

Traffic Display Enabled Icon
(Other Maps)

* See Table 6-16 for additional failure annunciations

FLIGHT
MANAGEMENT

Table 6-15 TIS Modes

Switching between TIS modes:
1) Select the Traffic Map Page.

HAZARD
AVOIDANCE

2) Press the STANDBY or OPERATE Softkey to switch between modes. The mode is displayed in the upper left
corner of the Traffic Map Page.

Or:
a) Press the MENU Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

b) Select ‘Operate Mode’ or ‘Standby Mode’ (choice dependent on current state) and press the ENT Key.

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Hazard Avoidance
SYSTEM
OVERVIEW

The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of
maps on which traffic can be displayed (Table 6-16).
Traffic Status Banner
Annunciation

TA X.X ± XX ↕

TRFC RMVD

Traffic is removed because it is too old for coasting (12 to 60 seconds since last message)
Traffic may exist within the selected display range, but it is not displayed
Traffic data has failed
Traffic has not been detected
The traffic service is unavailable or out of range

FLIGHT
MANAGEMENT

TRFC FAIL
NO TRFC DATA
TRFC UNAVAIL

AUDIO PANEL
& CNS

TRFC COAST

A Traffic Advisory is outside the selected display range*
Annunciation is removed when traffic comes within the selected display range
System cannot determine bearing of Traffic Advisory**
Annunciation indicates distance in nm, altitude separation in hundreds of feet, and
altitude trend arrow (climbing/descending)
Appears if traffic data is not refreshed within 6 seconds
If after another 6 seconds data is not received, traffic is removed from the display
The quality of displayed traffic information is reduced as the age increases
The displayed data is not current (6 to 12 seconds since last message)
The quality of displayed traffic information is reduced when this message is displayed

EIS

AGE MM:SS

FLIGHT
INSTRUMENTS

TA OFF SCALE

Description

*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page

HAZARD
AVOIDANCE

Table 6-16 TIS Traffic Status Annunciations

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance

6.7 Traffic Advisory System

FLIGHT
INSTRUMENTS

NOTE: TIS is disabled when Traffic Advisory System (TAS) is installed.

Refer to the Avidyne TAS600 Series Pilot’s Guide for a detailed discussion of the Avidyne TAS600.

TAS Symbology

EIS

Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses an onboard interrogator-processor and the Mode S transponder for the air-to-air traffic data link. Traffic is displayed
according to TCAS symbology using four different symbols.
TAS Symbol

Description

AUDIO PANEL
& CNS

Non-Threat Traffic

FLIGHT
MANAGEMENT

Proximity Advisory (PA)
Traffic Advisory (TA)
Traffic Advisory Off Scale

HAZARD
AVOIDANCE

Table 6-17 TAS Symbol Description

A Non-threat Advisory, shown as an open white diamond, indicates that an intruding aircraft is at greater than
±1200 feet relative altitude or the distance is beyond 5 nm.

AFCS

A Proximity Advisory indicates that the intruding aircraft is within ±1200 feet and is within 5 nm range, but
is still not considered a threat.

INDEX

APPENDICES

ADDITIONAL
FEATURES

A Traffic Advisory (TA) alerts the crew to a potentially hazardous intruding aircraft. Closing rate, distance,
and vertical separation meet TA criteria. A Traffic Advisory that is beyond the selected display range is indicated
by a half TA symbol at the edge of the screen at the relative bearing of the intruder.

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Hazard Avoidance
SYSTEM
OVERVIEW

Displaying Traffic Data
Traffic information is displayed on the following maps:
• Trip Planning Page

• Navigation Map Page

• Nearest Pages

• Traffic Map Page

• Active Flight Plan Page

FLIGHT
INSTRUMENTS

• PFD Inset Map

Displaying traffic on the Traffic Map Page:
EIS

1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.

Operating
Mode

AUDIO PANEL
& CNS

3) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area.

Traffic Display
Range

Altitude
Mode

FLIGHT
MANAGEMENT

Traffic Advisory,
Aircraft is
400’ Below,
Climbing

HAZARD
AVOIDANCE

“Non-Bearing”
Traffic (Bearing
Undetermined),
Distance 8.0 nm,
1100’ Above,
Descending

Proximity
Traffic, 1000’
Above,
Descending

AFCS

Off Scale
Traffic

ADDITIONAL
FEATURES

Figure 6-90 Traffic Map Page

APPENDICES

The Traffic Map Page shows surrounding TAS traffic data in relation to the aircraft’s current position and
altitude, without basemap clutter. Aircraft orientation is always heading up unless there is no valid heading.
Map range is adjustable with the RANGE Knob from 2 to 24 nm, as indicated by the map range rings.
The traffic mode and altitude display mode are annunciated in the upper left corner.

INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance
Displaying traffic information (maps other than the Traffic Map Page):
1) Press the MAP Softkey.

FLIGHT
INSTRUMENTS

2) Press the TRAFFIC Softkey to display traffic data.

When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate TAS is
enabled for display.

EIS

Traffic
Advisory

AUDIO PANEL
& CNS

Proximity
Traffic

FLIGHT
MANAGEMENT

Non-Threat
Traffic

HAZARD
AVOIDANCE

TA Off Scale
Banner
Non-Bearing
Traffic Advisories
Figure 6-91 TAS Traffic on Navigation Map

AFCS

Displaying traffic information (PFD Inset Map):
1) Press the INSET Softkey.

ADDITIONAL
FEATURES

2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1).
3) Press the softkey again to display the traffic-only inset (TRFC-2).

INDEX

APPENDICES

4) Press the softkey again to remove traffic data.

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Hazard Avoidance
SYSTEM
OVERVIEW

Altitude Display
Changing the altitude display mode:

FLIGHT
INSTRUMENTS

1) On the Traffic Page, press the ALT MODE Softkey.
2) Press one of the following Softkeys:
• BELOW

• NORMAL

• ABOVE

• UNREST (unrestricted)

EIS

3) To return to the Traffic Page, press the BACK Softkey.
Or:

AUDIO PANEL
& CNS

1) Press the MENU Key.
2) Turn the small FMS Knob to select one of the following:
• BELOW

• NORMAL

• ABOVE

• UNREST (unrestricted)

FLIGHT
MANAGEMENT

HAZARD
AVOIDANCE

3) Press the ENT Softkey.

Traffic Map Page Display Range
The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the
RANGE Knob from 2 to 24 nm, as indicated by the map range rings.

AFCS

Changing the display range on the Traffic Page:
1) Turn the RANGE Knob.
2) The following range options are available:

• 2 and 6 nm

• 6 and 12 nm

• 12 and 24 nm

APPENDICES

• 2 nm

ADDITIONAL
FEATURES

The Navigation Map Page Setup Menu also controls the display of traffic. The setup menu controls the map
range settings. Traffic data symbols and labels can be decluttered from the display. If a map range larger than
the map range setting is selected, the data is removed from the map. Maps besides the Traffic Map Page use
settings based on those selected for the Navigation Map Page.

INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance
Customizing the traffic display on the Navigation Map Page:
1) Select the Navigation Map Page.

FLIGHT
INSTRUMENTS

2) Press the MENU Key.
3) With Map Setup highlighted, press the ENT Key (Figure 6-92).
4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-93).
5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-94).
• TRAFFIC – Turns the display of traffic data on or off

AUDIO PANEL
& CNS

EIS

• TRAFFIC MODE – Selects the traffic mode for display; select from:

- All Traffic - Displays all traffic

- TA/PA - Displays Traffic Alerts and Proximity Advisories

- TA ONLY - Displays Traffic Alerts only

• TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown
• TRAFFIC LBL – Selects the maximum range at which traffic labels are shown with the option to turn off

FLIGHT
MANAGEMENT

6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings, etc.).
7) Press the ENT Key to select an option.

AFCS

HAZARD
AVOIDANCE

8) Press the FMS Knob or CLR Key to return to the Navigation Map Page.

APPENDICES

ADDITIONAL
FEATURES

Figure 6-92 Navigation Map Page Menu

Figure 6-94 Navigation Map Page Setup Menu, Traffic Group

INDEX

Figure 6-93 Navigation Map Page Setup Menu

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SYSTEM
OVERVIEW

TAS Alerts
NOTE: Refer to the TAS600 documentation for information on alerts generated by the TAS equipment.

FLIGHT
INSTRUMENTS

When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur:
• A “Traffic” voice alert is generated followed by the clock position, relative altitude and range of the TA.
• A TRAFFIC Annunciation appears at the top right of the airspeed on the PFD, flashing for 5 seconds and
remaining displayed until no TAs are detected in the area.

EIS

• The PFD Inset Map is automatically displayed with TA traffic.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Inset Map
Displays When
TA is Detected

HAZARD
AVOIDANCE

Figure 6-95 Traffic Annunciation (PFD)

TAS Voice Alerts
AFCS

To listen to an update of Traffic Advisories press the MUTE Softkey twice. If no Traffic Advisories (TAs) are
in effect, a “No Advisories” statement is heard.
Muting the TAS voice alert in progress:

ADDITIONAL
FEATURES

1) Select the Traffic Map Page.
2) Select the MUTE Softkey while the voice alert is playing. Subsequent voice alerts will be heard.

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Hazard Avoidance

System Status

FLIGHT
INSTRUMENTS

NOTE: Refer to the TAS600 documentation for information on the operating mode.

The traffic mode is annunciated in the upper left corner of the Traffic Map Page.
Traffic Mode Annunciation
(Traffic Map Page)

Mode

Traffic Display Enabled Icon
(Other Maps)

OPERATING

EIS

TAS Operating

FAIL

TAS Failed*
AUDIO PANEL
& CNS

* See Table 6-21 for additional failure annunciations
Table 6-18 TAS Modes

FLIGHT
MANAGEMENT

If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page.
Traffic Map Page
Annunciation
NO DATA

HAZARD
AVOIDANCE

DATA FAILED
FAILED

Description
Data is not being received from the TAS unit
Data is being received from the TAS unit, but the
unit is self-reporting a failure
Incorrect data format received from the TAS unit

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Table 6-19 TAS Failure Annunciations

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Hazard Avoidance
SYSTEM
OVERVIEW

The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of
maps on which traffic can be displayed.
Traffic Status Banner
Annunciation

NO TRFC DATA

AUDIO PANEL
& CNS

TRFC FAIL

EIS

TA X.X ± XX ↕

FLIGHT
INSTRUMENTS

TA OFF SCALE

Description

FLIGHT
MANAGEMENT

*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
Table 6-20 TAS Traffic Status Annunciations

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Hazard Avoidance

Blank Page

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Automatic Flight Control System
SYSTEM
OVERVIEW

Section 7 Automatic Flight Control System (Optional)

FLIGHT
INSTRUMENTS

Note: The approved Aircraft Flight Manual Supplement (AFMS) always supersedes the information in this

Pilot’s Guide.
Note: A failure of the primary (#1) Integrated Avionics Unit (IAU) results in loss of the flight director. Any

IAU failure results in loss of the autopilot and manual electric trim.

• GSA 81 AFCS Servo (3)

• GDU 1042/1044 Multi-Function Display (MFD)

• GSM 85 Servo Mounts (3)

AUDIO PANEL
& CNS

• GDU 1040 Primary Flight Display (PFD)

EIS

The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the G1000 System
avionics architecture. The System Overview section provides a block diagram (Figure 1-1) to support this
system description. GFC 700 AFCS functionality in Diamond DA40/40F aircraft is distributed across the
following Line Replaceable Units (LRUs):

• GIA 63/63W Integrated Avionics Units (2)

FLIGHT
MANAGEMENT

The GFC 700 AFCS can be divided into these main operating functions:
• Flight Director (FD) — Flight director operation takes place within the primary (#1) IAU. Flight director
commands are displayed on the PFD. The flight director provides:
– Command Bars showing pitch/roll guidance

HAZARD
AVOIDANCE

– Pitch/roll mode selection and processing
– Autopilot communication

AFCS

• Autopilot (AP) — Autopilot operation occurs within the pitch, roll, and pitch trim servo and provides servo
monitoring and automatic flight control in response to flight director steering commands, AHRS attitude and
rate information, and airspeed.
• Manual Electric Trim (MET) — The pitch trim servo provides manual electric trim capability when the
autopilot is not engaged.

ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

7.1 AFCS Controls

FLIGHT
INSTRUMENTS

The following dedicated AFCS keys are located on the bezel of the MFD:
1
2

AP Key
FD Key

Engages/disengages the autopilot
Activates/deactivates the flight director only
Pressing once turns on the flight director in the default pitch and roll modes. Pressing
again deactivates the flight director and removes the Command Bars. If the autopilot
is engaged, the key is disabled.
Selects/deselects Navigation Mode
Selects/deselects Altitude Hold Mode
Selects/deselects Vertical Speed Mode
Selects/deselects Flight Level Change Mode
Selects/deselects Heading Select Mode
Selects/deselects Approach Mode

NAV Key
4 ALT Key
5 VS Key
6 FLC Key
7 HDG Key
8 APR Key
9 VNV Key
Selects/deselects Vertical Path Tracking Mode for Vertical Navigation flight control
(GDU 1044
only)
10 NOSE UP/NOSE Control the mode reference in Pitch Hold, Vertical Speed, and Flight Level Change
modes
DN Keys

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

ADDITIONAL
FEATURES

AFCS

1
2

5
APPENDICES

10
6

INDEX

Figure 7-1 Dedicated MFD AFCS Controls (GDU 1044)

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Automatic Flight Control System
SYSTEM
OVERVIEW

The following AFCS controls are located in the cockpit separately from the MFD:
AP DISC Switch
(Autopilot Disconnect)

Disengages the autopilot and interrupts pitch trim operation

FLIGHT
INSTRUMENTS

This switch may be used to mute the aural autopilot disconnect alert.
The AP DISC Switch is located on each control stick.

While pressed, allows manual control of the aircraft while the autopilot is
CWS Button
(Control Wheel Steering) engaged and synchronizes the flight director’s Command Bars with the current
aircraft pitch (if not in Glideslope Mode) and roll (if in Roll Hold Mode)

EIS

Upon release of the CWS Button, the flight director may establish new
reference points, depending on the current pitch and roll modes. CWS
operation details are discussed in the flight director modes section.
GA Switch (Go Around)

AUDIO PANEL
& CNS

The CWS Button is located on the top of the left control stick.
Disengages the autopilot and selects flight director Go Around Mode

FLIGHT
MANAGEMENT

If an approach procedure is loaded this switch also activates the missed
approach when the selected navigation source is GPS or when the navigation
source is VOR/LOC and a valid frequency has been tuned.
The GA Switch is located on the throttle handle.
AP TRIM Switch
(Autopilot Trim)

Used to command manual electric trim

HAZARD
AVOIDANCE

This composite switch is split into left and right sides. The left switch is
the ARM contact and the right switch controls the DN (forward) and UP
(rearward) contacts. The AP TRIM ARM switch can be used to disengage
the autopilot and to acknowledge an autopilot disconnect alert and mute the
associated aural tone.

AFCS

Manual trim commands are generated only when both sides of the switch
are operated simultaneously. If either side of the switch is active separately for
more than three seconds, MET function is disabled and ‘PTRM’ is displayed
as the AFCS Status Annunciation on the PFD. The function remains disabled
until both sides of the switch are inactivated.

ADDITIONAL
FEATURES

The AP TRIM Switch is located on the left control stick.

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

7.2 Flight Director Operation

FLIGHT
INSTRUMENTS

The flight director function provides pitch and roll commands to the AFCS and displays them on the PFD.
With the flight director activated, the aircraft can be hand-flown to follow the path shown by the Command Bars.
Maximum commanded pitch (-15°/+20°) and roll (22°) angles, vertical acceleration, and roll rate are limited to
values established during AFCS certification. The flight director also provides commands to the autopilot.

Activating the Flight Director

EIS

An initial press of a key listed in Table 7-1 (when the flight director is not active) activates the flight director
in the listed modes. The flight director may be turned off and the Command Bars removed from the display by
pressing the FD Key again. The FD Key is disabled when the autopilot is engaged.

AUDIO PANEL
& CNS

Control Pressed

ALT Key
VS Key
VNV Key

Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Takeoff (on ground)
Go Around (in air)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)

NAV Key

Navigation**

APR Key

Approach**

HDG Key

Heading Select

FLIGHT
MANAGEMENT

FD Key
AP Key
CWS Button

AFCS

HAZARD
AVOIDANCE

GA Switch

ADDITIONAL
FEATURES

Modes Selected
ROL
ROL
ROL
TO
GA
ROL
ROL
ROL
GPS
VOR
LOC
BC
GPS
VOR
LOC
HDG

Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Takeoff (on ground)
TO
Go Around (in air)
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Pitch Hold (default)

PIT

Pitch Hold (default)

PIT

Pitch Hold (default)

PIT

*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS
course before NAV or APR Key press activates flight director.

INDEX

APPENDICES

Table 7-1 Flight Director Activation

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Automatic Flight Control System
SYSTEM
OVERVIEW

AFCS Status Box

Lateral Modes

Active

Vertical Modes

Active

Mode
Reference

Armed

EIS

Armed

Autopilot
Status

FLIGHT
INSTRUMENTS

Flight director mode annunciations are displayed on the PFD when the flight director is active. Autopilot
status is displayed in the center of the AFCS Status Box. Lateral flight director modes are displayed on the left
and vertical on the right. Armed modes are annunciated in white and active in green.

AFCS Status Box
AUDIO PANEL
& CNS

Selected
Altitude

FLIGHT
MANAGEMENT

Command
Bars

HAZARD
AVOIDANCE

GPS is
Selected
Navigation
Source

AFCS

Figure 7-2 PFD AFCS Display

ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

Command Bars

FLIGHT
INSTRUMENTS

Upon activation of the flight director, Command Bars are displayed on the PFD as a single magenta cue. The
Command Bars move together vertically to indicate pitch commands and bank left or right to indicate roll
commands. The Command Bars do not override the aircraft symbol.
If the attitude information sent to the flight director becomes invalid or unavailable, the Command Bars are
removed from the display. The flight director Command Bars also disappear if the pitch exceeds +30˚/-20˚ or
bank exceeds 65˚.

EIS

Command Bars

AUDIO PANEL
& CNS

Aircraft Symbol
Figure 7-3 Command Bars

FLIGHT
MANAGEMENT

Flight Director Modes
Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise
specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection,
the flight director reverts to the default pitch and/or roll mode(s).

HAZARD
AVOIDANCE

Armed modes are annunciated in white and active in green in the AFCS Status Box. Under normal operation,
when the control for the active flight director mode is pressed, the flight director reverts to the default mode(s)
for the axis(es). Automatic transition from armed to active mode is indicated by the white armed mode
annunciation moving to the green active mode field and flashing for 10 seconds.

ADDITIONAL
FEATURES

AFCS

If the information required to compute a flight director mode becomes invalid or unavailable, the flight
director automatically reverts to the default mode for that axis. A flashing yellow mode annunciation and
annunciator light indicate loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, WAAS) required to
compute commands. When such a loss occurs, the system automatically begins to roll the wings level (enters
Roll Hold Mode) or maintain the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The
flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected. If
after 10 seconds no action is taken, the flashing annunciation stops.

APPENDICES

Figure 7-4 Loss of VOR Signal

INDEX

The flight director is automatically disabled if the attitude information required to compute the default flight
director modes becomes invalid or unavailable.

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SYSTEM
OVERVIEW

7.3 Vertical Modes

Pitch Hold

Flight Level Change

VNV Target Altitude Capture
Glidepath***

-15° to +20°

0.5°

nnnn fpm

-3000 to
+1500 fpm

100 fpm

nnn kt

70 to 165 kt

1 kt

PIT

*
ALTS
ALT Key ALT nnnnn ft
VS Key

FLC Key FLC
VNV
Key

VPTH

ALTV

APR
Key
GA
Switch

GP
GS
GA

7°

ADDITIONAL
FEATURES

Go Around

(default)

AFCS

Glideslope

Reference
Change
Increment

HAZARD
AVOIDANCE

Vertical Path Tracking

Reference
Range

FLIGHT
MANAGEMENT

Vertical Speed

Holds aircraft pitch attitude; may
be used to climb/descend to the
Selected Altitude
Captures the Selected Altitude
Holds current Altitude Reference
Holds aircraft vertical speed; may
be used to climb/descend to the
Selected Altitude
Holds aircraft airspeed while
aircraft is climbing/descending to
the Selected Altitude
Captures and tracks descent legs
of an active vertical profile
Captures the Vertical Navigation
(VNV) Target Altitude
Captures and tracks the WAAS
glidepath on approach
Captures and tracks the ILS
glideslope on approach
Disengages the autopilot and
commands a constant pitch angle
and wings level

Control Annunciation

AUDIO PANEL
& CNS

Selected Altitude Capture
Altitude Hold

Description

EIS

Vertical Mode

FLIGHT
INSTRUMENTS

Table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is
displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes.
The NOSE UP/NOSE DN Keys can be used to change the vertical mode reference while operating under Pitch
Hold, Vertical Speed, or Flight Level Change Mode. Increments of change and acceptable ranges of values for
each of these references using the NOSE UP/NOSE DN Keys are also listed in the table.

* ALTS is armed automatically when PIT, VS, FLC, or GA is active, and under VPTH when the Selected Altitude is to be captured
instead of the VNV Target Altitude.

APPENDICES

** ALTV is armed automatically under VPTH when the VNV Target Altitude is to be captured instead of the Selected Altitude.
***GP is available in installations with GIA 63W IAUs when WAAS is available.
Table 7-2 Flight Director Vertical Modes

INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

Pitch Hold Mode (PIT)

FLIGHT
INSTRUMENTS

When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch
Hold Mode is indicated as the active pitch mode by the green annunciation ‘PIT’. This mode may be used for
climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is
automatically armed when Pitch Hold Mode is activated.

EIS

In Pitch Hold Mode, the flight director maintains a constant pitch attitude, the pitch reference. The pitch
reference is set to the aircraft pitch attitude at the moment of mode selection. If the aircraft pitch attitude
exceeds the flight director pitch command limitations, the flight director commands a pitch angle equal to the
nose-up/down limit.

Changing the Pitch Reference

AUDIO PANEL
& CNS

When operating in Pitch Hold Mode, the pitch reference can be adjusted by:
• Using the NOSE UP/NOSE DN Keys
• Pressing the CWS Button, hand-flying the aircraft to establish a new pitch reference, then releasing the
CWS Button

FLIGHT
MANAGEMENT

Pitch Hold
Mode Active

Selected Altitude
Capture Mode Armed

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Selected
Altitude

Command Bars Maintain
Desired Pitch Reference

INDEX

APPENDICES

Figure 7-5 Pitch Hold Mode

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OVERVIEW

Selected Altitude Capture Mode (ALTS)
Selected Altitude Capture Mode is automatically armed with activation of the following modes:
• Go Around

• Vertical Speed

• Vertical Path Tracking (if the Selected Altitude is to
be captured instead of the VNV Target Altitude)

• Flight Level Change

FLIGHT
INSTRUMENTS

• Pitch Hold

The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-5 for example).
The ALT Knob is used to set the Selected Altitude (shown above the Altimeter) until Selected Altitude Capture
Mode becomes active.

EIS
AUDIO PANEL
& CNS

As the aircraft nears the Selected Altitude, the flight director automatically transitions to Selected Altitude
Capture Mode with Altitude Hold Mode armed (Figure 7-6). This automatic transition is indicated by the green
‘ALTS’ annunciation flashing for up to 10 seconds and the appearance of the white ‘ALT” annunciation. The
Selected Altitude is shown as the Altitude Reference beside the ‘ALTS’ annunciation.

FLIGHT
MANAGEMENT

At 50 feet from the Selected Altitude, the flight director automatically transitions from Selected Altitude
Capture to Altitude Hold Mode and holds the Selected Altitude (shown as the Altitude Reference). As Altitude
Hold Mode becomes active, the white ‘ALT’ annunciation moves to the active pitch mode field and flashes green
for 10 seconds to indicate the automatic transition.
Altitude Reference
(in this case, equal to
Selected Altitude)

HAZARD
AVOIDANCE

Flash up to 10 sec, Indicating Automatic Transition

Figure 7-6 Automatic Mode Transitions During Altitude Capture
AFCS

Changing the Selected Altitude

ADDITIONAL
FEATURES

NOTE: Pressing the CWS Button while in Selected Altitude Capture Mode does not cancel the mode.

Use of the ALT Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes
the flight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new
Selected Altitude.

APPENDICES
INDEX

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OVERVIEW

Automatic Flight Control System

Altitude Hold Mode (ALT)

FLIGHT
INSTRUMENTS

Altitude Hold Mode can be activated by pressing the ALT Key; the flight director maintains the current aircraft
altitude (to the nearest 10 feet) as the Altitude Reference. The flight director’s Altitude Reference, shown in the
AFCS Status Box, is independent of the Selected Altitude, displayed above the Altimeter. Altitude Hold Mode
active is indicated by a green ‘ALT’ annunciation in the AFCS Status Box.
Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode (see
Figure 7-6). Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude
error is less than 50 feet. In this case, the Selected Altitude becomes the flight director’s Altitude Reference.

EIS

Changing the Altitude Reference
NOTE: Turning the ALT Knob while in Altitude Hold Mode changes the Selected Altitude, but not the flight

AUDIO PANEL
& CNS

director’s Altitude Reference, and does not cancel the mode.
With the CWS Button depressed, the aircraft can be hand-flown to a new Altitude Reference. When the
CWS Button is released at the desired altitude, the new altitude is established as the Altitude Reference.

FLIGHT
MANAGEMENT

Altitude Hold
Mode Active

Altitude
Reference

HAZARD
AVOIDANCE

Selected
Altitude

ADDITIONAL
FEATURES

AFCS

Selected
Altitude
Bug

Command Bars Hold Pitch Attitude
to Maintain Altitude Reference

INDEX

APPENDICES

Figure 7-7 Altitude Hold Mode

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Vertical Speed Mode (VS)

FLIGHT
INSTRUMENTS

In Vertical Speed Mode, the flight director acquires and maintains a Vertical Speed Reference. Current aircraft
vertical speed (to the nearest 100 fpm) becomes the Vertical Speed Reference at the moment of Vertical Speed
Mode activation. This mode may be used for climb or descent to the Selected Altitude (shown above the
Altimeter) since Selected Altitude Capture Mode is automatically armed when Vertical Speed Mode is selected.
When Vertical Speed Mode is activated by pressing the VS Key, ‘VS’ is annunciated in green in the AFCS Status
Box along with the Vertical Speed Reference. The Vertical Speed Reference is also displayed above the Vertical
Speed Indicator. A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on
the indicator.

EIS

Changing the Vertical Speed Reference

AUDIO PANEL
& CNS

The Vertical Speed Reference (shown both in the AFCS Status Box and above the Vertical Speed Indicator)
may be changed by:
• Using the NOSE UP/NOSE DN Keys
• Pressing the CWS Button, hand-flying the aircraft to attain a new Vertical Speed Reference, then releasing
the CWS Button

FLIGHT
MANAGEMENT

NOTE: If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed.

To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected
Altitude is reached.
Vertical Speed
Reference

Selected Altitude
Capture Mode
Armed

AFCS

Selected
Altitude

HAZARD
AVOIDANCE

Vertical Speed
Mode Active

Vertical
Speed
Reference

ADDITIONAL
FEATURES
APPENDICES

Vertical
Speed
Reference
Bug

Command Bars Indicate Climb to
Attain Vertical Speed Reference

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INDEX

Figure 7-8 Vertical Speed Mode

367

SYSTEM
OVERVIEW

Flight Level Change Mode (FLC)

FLIGHT
INSTRUMENTS

Flight Level Change Mode is selected by pressing the FLC Key. This mode acquires and maintains the
Airspeed Reference while climbing or descending to the Selected Altitude (shown above the Altimeter). When
Flight Level Change Mode is active, the flight director continuously monitors Selected Altitude, airspeed, and
altitude.

EIS

Automatic Flight Control System

The Airspeed Reference is set to the current airspeed upon mode activation. Flight Level Change Mode is
indicated by a green ‘FLC’ annunciation beside the Airspeed Reference in the AFCS Status Box. The Airspeed
Reference is also displayed directly above the Airspeed Indicator, along with a bug corresponding to the Airspeed
Reference along the tape.

NOTE: The Selected Altitude should be set before selecting Flight Level Change Mode.

AUDIO PANEL
& CNS

Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding
to the desired flight profile (climb or descent) while maintaining the Airspeed Reference. The flight director
maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not
allow the aircraft to climb or descend away from the Selected Altitude.

FLIGHT
MANAGEMENT

Changing the Airspeed Reference
The Airspeed Reference (shown in both the AFCS Status Box and above the Airspeed Indicator) may be
adjusted by:
• Using the NOSE UP/NOSE DN Keys

HAZARD
AVOIDANCE

• Pressing the CWS Button, hand-flying the aircraft to a new airspeed, then releasing the CWS Button to
establish the new Airspeed Reference
NOTE: If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected
Altitude is reached.

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Automatic Flight Control System

Selected Altitude
Capture Mode
Armed

Airspeed
Reference

FLIGHT
INSTRUMENTS

Airspeed
Reference

SYSTEM
OVERVIEW

Flight Level Change
Mode Active

Airspeed
Reference
EIS
AUDIO PANEL
& CNS

Airspeed
Reference
Bug

FLIGHT
MANAGEMENT

Command Bars Indicate Climb
to Attain Selected Altitude
Figure 7-9 Flight Level Change Mode

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

Vertical Navigation Modes (VPTH, ALTV)

FLIGHT
INSTRUMENTS

Note: VNV is disabled when parallel track or dead reckoning mode is active.
Note: The Selected Altitude takes precedence over any other vertical constraints.

Vertical Navigation (VNV) flight control is available for enroute/terminal cruise and descent operations any
time that VNV flight planning is available. Refer to the Flight Management Section for more information on
VNV flight plans. Conditions for availability include, but are not limited to:

EIS

• The selected navigation source is GPS.
• A VNV flight plan (with at least one altitude-constrained waypoint) or vertical direct-to is active.

AUDIO PANEL
& CNS

• VNV is enabled (VNV ENBL Softkey pressed on the MFD).
• Crosstrack error is valid and within certain limits.
• Desired/actual track are valid or track angle error is within certain limits.

FLIGHT
MANAGEMENT

• The VNV Target Altitude of the active waypoint is no more than 250 ft above the current aircraft altitude.

HAZARD
AVOIDANCE

The flight director may be armed for VNV at any time, but no target altitudes are captured during a climb.
The Command Bars provide vertical profile guidance based on specified altitudes (entered manually or loaded
from the database) at waypoints in the active flight plan or vertical direct-to. The appropriate VNV flight control
modes are sequenced by the flight director to follow the path defined by the vertical profile. Upon reaching
the last waypoint in the VNV flight plan, the flight director transitions to Altitude Hold Mode and cancels any
armed VNV modes.

Vertical Path Tracking Mode (VPTH)
Note: If another pitch mode key is pressed while Vertical Path Tracking Mode is selected, Vertical Path

AFCS

Tracking Mode reverts to armed.
NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The

ADDITIONAL
FEATURES

autopilot guides the aircraft back to the descent path upon release of the CWS Button.

INDEX

APPENDICES

When a vertical profile (VNV flight plan) is active and the VNV Key is pressed, Vertical Path Tracking
Mode is armed in preparation for descent path capture. ‘VPTH’ (or ‘/V’ when Glidepath or Glideslope Mode
is concurrently armed) is annunciated in white in addition to previously armed modes. If applicable, the
appropriate altitude capture mode is armed for capture of the next VNV Target Altitude (ALTV) or the Selected
Altitude (ALTS), whichever is greater.

Figure 7-10 Vertical Path Tracking Armed Annunciations

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OVERVIEW

Prior to descent path interception, the Selected Altitude must be set below the current aircraft altitude
by at least 75 feet. For the flight director to transition from Altitude Hold to Vertical Path Tracking Mode,
acknowledgment is required within 5 minutes of descent path interception by:

FLIGHT
INSTRUMENTS

• Adjusting the Selected Altitude

• Pressing the VNV Key

If acknowledgment is not received within 1 minute of descent path interception, the white ‘VPTH’
annunciation starts to flash. Flashing continues until acknowledged or the descent path is intercepted. If
the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the
descent is not captured.

Vertical Path Tracking
Armed, (Flashing Indicates
Acknowledgment Required)

FLIGHT
MANAGEMENT

Selected
Altitude Below
VNV Target

AUDIO PANEL
& CNS

Altitude Hold
Mode Active

EIS

In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Status Box
and the “Vertical track” voice message, VNV indications (VNV Target Altitude, vertical deviation, and vertical
speed required) appear on the PFD in magenta (Figure 7-11).

VNV Target
Altitude

HAZARD
AVOIDANCE

Vertical
Deviation
Indicator
Required
Vertical
Speed Bug

AFCS

Terminal
Phase
of Flight

ADDITIONAL
FEATURES

GPS is
Selected
Navigation
Source

Figure 7-11 Vertical Path Capture

APPENDICES
INDEX

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OVERVIEW

Automatic Flight Control System
When a descent leg is captured (i.e., vertical deviation becomes valid), Vertical Path Tracking becomes
active and tracks the descent profile. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate.

FLIGHT
INSTRUMENTS

Vertical Path
Tracking Active

VNV Target Altitude
Capture Armed

AUDIO PANEL
& CNS

EIS

VNV Target
Altitude

FLIGHT
MANAGEMENT

GPS is
Selected
Navigation
Source

Terminal
Phase of
Flight

Required
Vertical
Speed
Indication

Command Bars Indicate Descent to
Maintain Required Vertical Speed
Vertical
Deviation
Indicator

HAZARD
AVOIDANCE

Figure 7-12 Vertical Path Tracking Mode

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

If the Altimeter’s barometric setting is adjusted while Vertical Path Tracking is active, the flight director
increases/decreases the descent rate by up to 500 fpm to re-establish the aircraft on the descent path (without
commanding a climb). Adjusting the altimeter barometric setting creates discontinuities in VNV vertical
deviation, moving the descent path. For large adjustments, it may take several minutes for the aircraft to reestablish on the descent path. If the change is made while nearing a waypoint with a VNV Target Altitude,
the aircraft may not re-establish on the descent path in time to meet the vertical constraint.

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SYSTEM
OVERVIEW

Automatic Reversion to Pitch Hold Mode
Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to
revert to Pitch Hold Mode:

FLIGHT
INSTRUMENTS

• Vertical deviation exceeds 200 feet during an overspeed condition.
• Vertical deviation experiences a discontinuity that both exceeds 200 feet in magnitude and results in the
vertical deviation exceeding 200 feet in magnitude. Such discontinuities are usually caused by flight plan
changes that affect the vertical profile.
• Vertical deviation becomes invalid (the Vertical Deviation Indicator is removed from the PFD).

EIS

• A display enters Reversionary Mode (this does not apply to an active vertical direct-to).
Unless VNV is disabled, Vertical Path Tracking Mode and the appropriate altitude capture mode become
armed following the reversion to Pitch Hold Mode to allow for possible profile recapture.

AUDIO PANEL
& CNS

Non-Path Descents

FLIGHT
MANAGEMENT

Pitch Hold, Vertical Speed, and Flight Level Change modes can also be used to fly non-path descents
while VNV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is
selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to
allow profile re-capture.

Figure 7-13 Flight Level Change VNV Non-Path Descent
HAZARD
AVOIDANCE

To prevent immediate profile re-capture, the following must be satisfied:
• At least 10 seconds have passed since the non-path transition was initiated
• Vertical deviation from the profile has exceeded 250 feet, but is now less than 200 feet

AFCS

Pressing the VNV Key twice re-arms Vertical Path Tracking for immediate profile re-capture.

ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System
VNV Target Altitude Capture Mode (ALTV)
Note: Armed VNV Target Altitude and Selected Altitude capture modes are mutually exclusive. However,

FLIGHT
INSTRUMENTS

Selected Altitude Capture Mode is armed implicitly (not annunciated) whenever VNV Target Altitude Capture
Mode is armed.

EIS

VNV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically
after the VNV Key is pressed and the next VNV Target Altitude is to be intercepted before the Selected
Altitude. The annunciation ‘ALTV’ indicates that the VNV Target Altitude is to be captured. VNV Target
Altitudes are shown in the active flight plan or vertical direct-to, and can be entered manually or loaded
from a database (see the Flight Management Section for details). At the same time as “TOD within 1 minute”
is annunciated in the Navigation Status Box, the active VNV Target Altitude is displayed above the Vertical
Speed Indicator (see Figure 7-11).

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

As the aircraft nears the VNV Target Altitude, the flight director automatically transitions to VNV Target
Altitude Capture Mode with Altitude Hold Mode armed. This automatic transition is indicated by the green
‘ALTV’ annunciation flashing for up to 10 seconds and the appearance of the white ‘ALT” annunciation. The
VNV Target Altitude is shown as the Altitude Reference beside the ‘ALTV’ annunciation and remains displayed
above the Vertical Speed Indicator. The Required Vertical Speed Indication (RVSI) is removed once VNV
Target Altitude Capture Mode becomes active.

HAZARD
AVOIDANCE

At 50 feet from the VNV Target Altitude, the flight director automatically transitions from VNV Target
Altitude Capture to Altitude Hold Mode and tracks the level leg. As Altitude Hold Mode becomes active, the
white ‘ALT’ annunciation moves to the active vertical mode field and flashes green for 10 seconds to indicate
the automatic transition. The flight director automatically arms Vertical Path Tracking, allowing upcoming
descent legs to be captured and subsequently tracked.

AFCS

Altitude Reference (In
This Case, Equal To
VNV Altitude Target)

Flash up to 10 sec, Indicating Automatic Transition

ADDITIONAL
FEATURES

Figure 7-14 Automatic Mode Transitions During Altitude Capture

Changing the VNV Target Altitude

APPENDICES

NOTE: Pressing the CWS Button while in VNV Target Altitude Capture Mode does not cancel the mode.

INDEX

Changing the current VNV Target Altitude while VNV Target Altitude Capture Mode is active causes the
flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture
mode are armed in preparation to capture the new VNV Target Altitude or the Selected Altitude, depending
on which altitude is to be intercepted first.
VNV target altitudes can be changed while editing the active flight plan (see the Flight Management
Section for details).

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SYSTEM
OVERVIEW

Glidepath Mode (GP) (WAAS only)
NOTE: Pressing the CWS Button while Glidepath Mode is active does not cancel the mode. The autopilot

FLIGHT
INSTRUMENTS

guides the aircraft back to the glidepath upon release of the CWS Button.

Glidepath Mode is available only in installations with GIA 63W IAUs when WAAS is available. Glidepath
Mode is used to track the WAAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white
in the AFCS Status Box.
Selecting Glidepath Mode:

EIS

1) Ensure a GPS approach with vertical guidance or vertical descent angle (LPV, LNAV/VNAV, LNAV+V) is loaded
into the active flight plan. The active waypoint must be part of the flight plan (cannot be a direct-to a waypoint
not in the flight plan.

AUDIO PANEL
& CNS

2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources).
3) Press the APR Key.
NOTE: Some RNAV (GPS) approaches provide a vertical descent angle as an aid in flying a stabilized

FLIGHT
MANAGEMENT

approach. These approaches are NOT considered Approaches with Vertical Guidance (APV). Approaches
that are annunciated on the HSI as LNAV or LNAV+V are considered Nonprecision Approaches (NPA) and
are flown to an MDA even though vertical glidepath (GP) information may be provided.
WARNING: When flying an LNAV approach (with vertical descent angle) with the autopilot coupled, the

HAZARD
AVOIDANCE

aircraft will not level off at the MDA even if the MDA is set in the altitude preselect.
Upon reaching the glidepath, the flight director transitions to Glidepath Mode and begins to capture and
track the glidepath.
Figure 7-15 Glidepath Mode Armed

AFCS

Once the following conditions have been met, the glidepath can be captured:
• The active waypoint is at or after the final approach fix (FAF)

ADDITIONAL
FEATURES

• Vertical deviation is valid
• The CDI is at less than full scale deviation
• Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI)

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

Glidepath
Mode Active

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

GPS Approach
Mode Active

FLIGHT
MANAGEMENT

GPS is Selected
Navigation
Source

LNAV
Approach
Active

Command Bars Indicate
Descent on Glidepath

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Figure 7-16 Glidepath Mode

Glidepath
Indicator

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SYSTEM
OVERVIEW

Glideslope Mode (GS)
NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot

FLIGHT
INSTRUMENTS

guides the aircraft back to the glideslope upon release of the CWS Button.

Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope
Mode is armed (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the lateral flight director
mode.
Selecting Glideslope Mode:

EIS

1) Ensure a valid localizer frequency is tuned.
2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources).
3) Press the APR Key.
Or:

AUDIO PANEL
& CNS

1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources).
2) Ensure a LOC/ILS approach is loaded into the active flight plan.

FLIGHT
MANAGEMENT

3) Ensure the corresponding LOC frequency is tuned.
4) Press the APR Key.
Figure 7-17 Glideslope Mode Armed

Active ILS
Frequency Tuned

Approach
Mode Active

HAZARD
AVOIDANCE

Once LOC is the navigation source, the localizer and glideslope can be captured. Upon reaching the glideslope,
the flight director transitions to Glideslope Mode and begins to capture and track the glideslope.
Glideslope
Mode Active

AFCS
ADDITIONAL
FEATURES

Command Bars Indicate Descent
on Localizer/Glideslope Path

Garmin G1000 Pilot’s Guide for Diamond DA40/40F

Glideslope
Indicator

INDEX

Figure 7-18 Glideslope Mode

190-00592-06 Rev. A

APPENDICES

NAV2 (localizer) is Selected
Navigation Source

377

SYSTEM
OVERVIEW

Automatic Flight Control System

Go Around Mode (GA)

FLIGHT
INSTRUMENTS

Pushing the GA Switch engages the flight director in a wings-level, pitch-up attitude, allowing the execution
of a missed approach or a go around. This mode is a coupled pitch and roll mode and is annunciated as ‘GA’
in both the active pitch and roll mode fields. Go Around Mode disengages the autopilot and arms Selected
Altitude Capture Mode automatically. Subsequent autopilot engagement is allowed. Attempts to modify the
aircraft attitude (i.e., with the CWS Button or NOSE UP/NOSE DN Keys) result in reversion to Pitch and Roll
Hold modes.

EIS

Go Around Mode Active

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Autopilot Disconnect Annunciation
Flashes Yellow 5 sec

Command Bars Indicate Climb

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 7-19 Go Around Mode

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SYSTEM
OVERVIEW

7.4 Lateral Modes

Lateral Mode

Description

Control Annunciation

Roll Hold

Heading Select

Navigation, VOR Enroute Capture/Track

Navigation Backcourse Capture/Track

HDG

22º

GPS

22º
22º Capture
10º Track
22º Capture
10º Track

VOR
NAV
Key

Captures and tracks a
localizer signal for backcourse
approaches

LOC
BC

Approach, GPS

GPS

Approach, LOC Capture/Track
(Glideslope Mode automatically armed)

Captures and tracks the
selected navigation source (GPS,
VOR, LOC)

VAPP
LOC

GA
Switch

22º
22º Capture
10º Track
22º Capture
10º Track
Wings Level

AFCS

Disengages the autopilot and
commands a constant pitch
angle and wings level

APR
Key

22º Capture
10º Track

HAZARD
AVOIDANCE

Approach, VOR Capture/Track

Go Around

22º

FLIGHT
MANAGEMENT

Navigation, LOC Capture/Track
(No Glideslope)

Captures and tracks the
selected navigation source (GPS,
VOR, LOC)

ROL

AUDIO PANEL
& CNS

Navigation, GPS

Maximum Roll
Command Limit

EIS

Holds the current aircraft roll
attitude or rolls the wings level,
(default)
depending on the commanded
bank angle
Captures and tracks the
HDG
Selected Heading
Key

FLIGHT
INSTRUMENTS

The GFC 700 offers the lateral modes listed in Table 7-3. Refer to the vertical modes section for information
regarding Go Around Mode.

The GFC 700 limits turn rate to 3 degrees per second (standard rate turn).
ADDITIONAL
FEATURES

Table 7-3 Flight Director Lateral Modes

The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach
modes. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS
Button.

APPENDICES
INDEX

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Automatic Flight Control System

Roll Hold Mode (ROL)
Note: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls the wings

FLIGHT
INSTRUMENTS

level.

EIS

When the flight director is activated, Roll Hold Mode is selected by default. This mode is annunciated as
‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle conditions listed
in Table 7-4.

Figure 7-20 Roll Hold Mode Annunciation

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Bank Angle
< 6°
6 to 22°
> 22°

Flight Director Response
Rolls wings level
Maintains current aircraft roll attitude
Limits bank to 22°

Table 7-4 Roll Hold Mode Responses

Changing the Roll Reference

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

The roll reference can be changed by pressing the CWS Button, establishing the desired bank angle, then
releasing the CWS Button.

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SYSTEM
OVERVIEW

Heading Select Mode (HDG)

FLIGHT
INSTRUMENTS

Heading Select Mode is activated by pressing the HDG Key. Heading Select Mode acquires and maintains the
Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper
left of the HSI.

Changing the Selected Heading
Note: Pressing the HDG Knob synchronizes the Selected Heading to the current heading.

EIS

The Selected Heading is adjusted using the HDG Knob. Pressing the CWS Button and hand-flying the
aircraft does not change the Selected Heading. The autopilot guides the aircraft back to the Selected Heading
upon release of the CWS Button.

Heading Select
Mode Active

AUDIO PANEL
& CNS

Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned
more than 180° from the present heading (e.g., a 270° turn to the right). However, Selected Heading changes
of more than 340° at a time result in turn reversals.
Pitch Mode
Active

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

Selected
Heading
Bug

ADDITIONAL
FEATURES

Selected
Heading

Command Bars Track
Selected Heading

Figure 7-21 Heading Select Mode
APPENDICES
INDEX

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OVERVIEW

Automatic Flight Control System

Navigation Modes (GPS, VOR, LOC, BC)
NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the

FLIGHT
INSTRUMENTS

flight director to enter Navigation Mode.
NOTE: When intercepting a flight plan leg, the flight director gives commands to capture the active leg at

EIS

approximately a 45° angle to the track between the waypoints defining the active leg. The flight director
does not give commands fly to the starting waypoint of the active leg.
NOTE: When making a backcourse approach, set the Selected Course to the localizer front course.

AUDIO PANEL
& CNS

Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation
source (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected
navigation source. When the navigation source is VOR or LOC, the flight director creates roll steering commands
from the Selected Course and deviation. Navigation Mode can also be used to fly non-precision GPS and LOC
approaches where glideslope capture is not required.

FLIGHT
MANAGEMENT

Backcourse Navigation Mode is selected when the localizer front course is greater than 105° from the aircraft
heading. Backcourse Navigation Mode captures and tracks a localizer signal in the backcourse direction. The
annunciation ‘BC’ in the AFCS Status Box indicates Backcourse Navigation Mode.

HAZARD
AVOIDANCE

If the Course Deviation Indicator (CDI) shows greater than one dot when the NAV Key is pressed, the selected
mode is armed. If the CDI is less than one dot, Navigation Mode is automatically captured when the NAV Key
is pressed. The armed annunciation appears in white to the left of the active roll mode.

Figure 7-22 GPS Navigation Mode Armed

ADDITIONAL
FEATURES

AFCS

When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation
Mode remains active, providing GPS steering guidance until the localizer signal is captured. LOC Navigation
Mode is armed automatically when the navigation source switch takes place if the APR Key is not pressed prior
to the automatic source switch.
If Navigation Mode is active and either of the following occur, the flight director reverts to Roll Hold Mode
(wings rolled level):
• Different VOR tuned while in VOR Navigation Mode (VOR Navigation Mode reverts to armed)

APPENDICES

• Navigation source manually switched (with the CDI Softkey)

INDEX

• During a LOC/ILS approach the FAF is crossed while in GPS Navigation Mode after the automatic navigation
source switch from GPS to LOC

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SYSTEM
OVERVIEW

Changing the Selected Course

Selected Altitude
Capture Mode
Armed

Pitch Mode
Active

GPS Navigation
Mode Active

FLIGHT
INSTRUMENTS

The Selected Course is controlled using the CRS Knob (while in VOR, LOC, or OBS Mode). Pressing the
CWS Button and hand-flying the aircraft does not change the Selected Course while in Navigation Mode.
The autopilot guides the aircraft back to the Selected Course (or GPS flight plan) when the CWS Button is
released.

EIS
AUDIO PANEL
& CNS

Command Bars Indicate Left
Turn to Track GPS Course and Climb
to Intercept Selected Altitude

HAZARD
AVOIDANCE

Selected
Course

FLIGHT
MANAGEMENT

GPS is Selected
Navigation
Source

Figure 7-23 Navigation Mode
Backcourse
Mode Active

Pitch Hold
Mode Active
AFCS
ADDITIONAL
FEATURES
APPENDICES

Command Bars Hold Pitch Attitude
INDEX

LOC2 is Selected Navigation Source

Figure 7-24 Backcourse Mode

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Automatic Flight Control System

Approach Modes (GPS, VAPP, LOC)
NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the

FLIGHT
INSTRUMENTS

flight director to enter Approach Mode.
Approach Mode is activated when the APR Key is pressed. Approach Mode acquires and tracks the selected
navigation source (GPS, VOR, or LOC), depending on loaded approach. This mode uses the selected navigation
receiver deviation and desired course inputs to fly the approach. Pressing the APR Key when the CDI is greater
than one dot arms the selected approach mode (annunciated in white to the left of the active lateral mode). If
the CDI is less than one dot, the LOC is automatically captured when the APR Key is pressed.

EIS

VOR Approach Mode (VAPP) provides greater sensitivity for signal tracking than VOR Navigation Mode.
Selecting VOR Approach Mode:

AUDIO PANEL
& CNS

1) Ensure a valid VOR frequency is tuned
2) Ensure that VOR is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).

FLIGHT
MANAGEMENT

3) Press the APR Key.

When GPS Approach Mode is armed, Glidepath Mode is also armed.
Selecting GPS Approach Mode:

HAZARD
AVOIDANCE

1) Ensure a GPS approach is loaded into the active flight plan. The active waypoint must be part of the flight plan
(cannot be a direct-to a waypoint not in the flight plan).
2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).

AFCS

3) Press the APR Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 7-25 GPS Approach Mode Armed

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SYSTEM
OVERVIEW

LOC Approach Mode allows the autopilot to fly a LOC/ILS approach with a glideslope. When LOC Approach
Mode is armed, Glideslope Mode is also armed automatically. LOC captures are inhibited if the difference
between aircraft heading and localizer course exceeds 105°.

FLIGHT
INSTRUMENTS

Selecting LOC Approach Mode:
1) Ensure a valid localizer frequency is tuned.
2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).
3) Press the APR Key.
Or:

EIS

1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).
AUDIO PANEL
& CNS

2) Ensure a LOC/ILS approach is loaded into the active flight plan.
3) Ensure the corresponding LOC frequency is tuned.
4) Press the APR Key.

FLIGHT
MANAGEMENT

If the following occurs, the flight director reverts to Roll Hold Mode (wings rolled level):
• Approach Mode is active and a Vectors-To-Final is activated
• Approach Mode is active and Navigation source is manually switched

HAZARD
AVOIDANCE

• During a LOC/ILS approach, GPS Navigation Mode is active and the FAF is crossed after the automatic
navigation source switch from GPS to LOC

Changing the Selected Course

AFCS

The Selected Course is controlled using the CRS Knob (while in VOR, LOC, or OBS Mode). Pressing the
CWS Button and hand-flying the aircraft does not change the Selected Course while in Approach Mode.
The autopilot guides the aircraft back to the Selected Course (or GPS flight plan) when the CWS Button is
released.

ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

7.5 Autopilot Operation

FLIGHT
INSTRUMENTS

NOTE: Refer to the AFM for specific instructions regarding emergency procedures.

The autopilot operates flight control surface servos to provide automatic flight control. Pitch and roll commands
are provided to the servos, based on the active flight director modes. The autopilot uses pitch and roll rates to
stabilize the aircraft attitude during upsets and flight director maneuvers. Flight director commands are rate- and
attitude-limited, combined with pitch and roll damper control, and sent to the pitch and roll servo motors.

EIS

Pitch autotrim provides trim commands to the pitch trim servo to relieve any sustained effort required by the
pitch servo. The pitch servo measures the output effort (torque) and provides this signal to the pitch trim servo.
The pitch trim servo commands the motor to reduce the average pitch servo effort.

AUDIO PANEL
& CNS

When the autopilot is not engaged, the pitch trim servo may be used to provide manual electric trim (MET).
This allows the aircraft to be trimmed using a control wheel switch rather than the trim wheel. Manual trim
commands are generated only when both halves of the AP TRIM Switch are operated simultaneously. Trim
speeds are scheduled with airspeed to provide more consistent response.

FLIGHT
MANAGEMENT

Servo motor control limits the maximum servo speed and torque. The servo mounts are equipped with slipclutches set to certain values. This allows the servos to be overridden in case of an emergency.

Engaging the Autopilot
NOTE: Autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use

HAZARD
AVOIDANCE

the CWS Button to disengage the pitch and roll servos while the autopilot remains active.

When the AP Key is pressed, the autopilot and flight director (if not already engaged) are activated. Engagement
is indicated by a green ‘AP’ annunciation in the center of the AFCS Status Box. The flight director engages in
Pitch and Roll Hold modes when initially activated.

AFCS

Autopilot
Engaged

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 7-26 Autopilot and Yaw Damper Engaged

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SYSTEM
OVERVIEW

Control Wheel Steering

FLIGHT
INSTRUMENTS

During autopilot operation, the aircraft may be hand-flown without disengaging the autopilot. Pressing and
holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the
aircraft to be hand-flown. At the same time, the flight director is synchronized to the aircraft attitude during
the maneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS
maneuvers.
In most scenarios, releasing the CWS Button reengages the autopilot with a new reference. Refer to the flight
director modes section for specific CWS behavior in each mode.

EIS

Control Wheel Steering

AUDIO PANEL
& CNS

Figure 7-27 CWS Annunciation

Disengaging the Autopilot

FLIGHT
MANAGEMENT

The autopilot is manually disengaged by pushing the AP DISC Switch, GA Switch, AP TRIM ARM Switch, or
the AP Key on the MFD. Manual disengagement is indicated by a five-second flashing yellow ‘AP’ annunciation
and a two-second autopilot disconnect aural alert. After manual disengagement, the autopilot disconnect aural
alert may be cancelled by pushing the AP TRIM ARM or AP DISC Switch (AP DISC Switch also cancels the
flashing ‘AP’ annunciation).

HAZARD
AVOIDANCE

Figure 7-28 Manual Autopilot Disengagement

• System failure

AFCS

Automatic autopilot disengagement is indicated by a flashing red ‘AP’ annunciation and by the autopilot
disconnect aural alert, which continue until acknowledged by pushing the AP DISC or AP TRIM ARM Switch.
Automatic disengagement occurs due to:
• Invalid sensor data

ADDITIONAL
FEATURES

• Inability to compute default flight director modes
(FD also disengages automatically)

Figure 7-29 Automatic Autopilot Disengagement
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

7.6 Example Flight Plan

FLIGHT
INSTRUMENTS

Note: The following example flight plan and diagrams (not to be used for navigation) in this section are

for instructional purposes only and should be considered not current. Numbered portions of accompanying
diagrams correspond to numbered procedure steps.

EIS

This scenario-based set of procedures (based on the example flight plan found in the Flight Management
Section) shows various GFC 700 AFCS modes used during a flight. In this scenario, the aircraft departs Charles
B. Wheeler Downtown Airport (KMKC), enroute to Colorado Springs Airport (KCOS). After departure, the
aircraft climbs to 12,000 ft and airway V4 is intercepted, following ATC vectors.

Lamar
VOR
(LAA)

Topeka
VOR
(TOP)
21

Hays
VOR
(HYS)

V 244

Salina
VOR
(SLN)

V 244

KMKC

KCOS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

33
0

AUDIO PANEL
& CNS

Airway V4 is flown to Salina VOR (SLN) using VOR navigation, then airway V244 is flown using GPS navigation.
The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach
is executed.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 7-30 Flight Plan Overview

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SYSTEM
OVERVIEW

Departure
Climbing to the Selected Altitude and flying an assigned heading:

FLIGHT
INSTRUMENTS

1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob.
2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or
Flight Level Change Mode may be used).
a) Press the VS Key to activate Vertical Speed Mode.

EIS
AUDIO PANEL
& CNS

The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/
NOSE DN Keys or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed
Reference.
b) Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode.

FLIGHT
MANAGEMENT

3) Use the HDG Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4.

Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot
follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading.

HAZARD
AVOIDANCE

4) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.

AFCS

At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation flashes for up to 10 seconds; the autopilot
transitions to Altitude Hold Mode and levels the aircraft.

ADDITIONAL
FEATURES
APPENDICES
INDEX

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EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Automatic Flight Control System

AUDIO PANEL
& CNS

FLIGHT
MANAGEMENT

Selected Altitude of 12,000 MSL
ALT Mode

4
KMKC

HAZARD
AVOIDANCE

Mod

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 7-31 Departure

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Automatic Flight Control System
SYSTEM
OVERVIEW

Intercepting a VOR Radial

FLIGHT
INSTRUMENTS

During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina
VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight
director Navigation Mode using either VOR or GPS as the navigation source may be used. In this scenario, VOR
Navigation Mode is used for navigation to the first VOR waypoint in the flight plan.
Intercepting a VOR radial:
1) Arm VOR Navigation Mode:
a) Tune the VOR frequency.

EIS

b) Press the CDI Softkey to set the navigation source to VOR.

AUDIO PANEL
& CNS

c) Use the CRS Knob to set the Selected Course to 255°. Note that at this point, the flight director is still in
Heading Select Mode and the autopilot continues to fly 290°.
d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of
the active lateral mode.

FLIGHT
MANAGEMENT

2) As the aircraft nears the Selected Course, the flight director transitions from Heading Select to VOR Navigation
Mode and the ‘VOR’ annunciation flashes green. The autopilot begins turning to intercept the Selected
Course.

HAZARD
AVOIDANCE

3) The autopilot continues the turn until the aircraft is established on the Selected Course.
0

AFCS

Hd
29 g
0o

Salina
VOR
(SLN)

NA
V

2
HD

ADDITIONAL
FEATURES

255

VO
R

APPENDICES

21
18

Figure 7-32 Intercepting a VOR Radial

INDEX

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SYSTEM
OVERVIEW

Automatic Flight Control System

Flying a Flight Plan/GPS Course
Note: Changing the navigation source cancels Navigation Mode and causes the flight director to revert

FLIGHT
INSTRUMENTS

back to Roll Hold Mode (wings rolled level).
As the aircraft closes on Salina VOR, GPS is used to navigate the next leg, airway V244. The aircraft is
currently tracking inbound on Airway V4.
Flying a GPS flight plan:

EIS

1) Transition from VOR to GPS Navigation Mode:
a) Press the CDI Softkey until GPS is the selected navigation source.

AUDIO PANEL
& CNS

b) Press the NAV Key to activate GPS Navigation Mode. The autopilot guides the aircraft along the active flight
plan leg.

FLIGHT
MANAGEMENT

2) Following the flight plan, the autopilot continues to steer the aircraft under GPS guidance. Note that in GPS
Navigation Mode, course changes defined by the flight plan are automatically made without pilot action
required.
0

0
3

HAZARD
AVOIDANCE

075

d
AV Mo

GPS N

260

ADDITIONAL
FEATURES

AFCS

Hays
VOR
(HYS)

Salina
VOR
(SLN)

V 244

076

d
AV Mo

VOR N

INDEX

APPENDICES

Figure 7-33 Transition to GPS Flight Plan

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SYSTEM
OVERVIEW

Descent
While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS.
Three methods are presented for the descent:

FLIGHT
INSTRUMENTS

• Flight Level Change descent – Flight Level Change Mode can be used to descend to the Selected Altitude at a
constant airspeed. This descent method does not account for flight plan waypoint altitude constraints.
• Vertical Path Tracking descent – Vertical Path Tracking Mode is used to follow the vertical descent path
defined in the GPS flight plan. Altitude constraints correspond to waypoints in the flight plan. Before VNV
flight control can provide vertical profile guidance, a VNV flight plan must be entered and enabled.

EIS

• Non-path descent in a VNV scenario – A VNV flight plan is entered and enabled, however Pitch Hold, Vertical
Speed, or Flight Level Change Mode can be used to descend to the VNV Target Altitude prior to reaching the
planned TOD. Flight Level Change Mode is used in the example.

AUDIO PANEL
& CNS

Flight Level Change descent:
1) Select Flight Level Change Mode:
a) Using the ALT Knob, set the Selected Altitude to 10,000 feet.

FLIGHT
MANAGEMENT

b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the
Airspeed Reference, which defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed
automatically.

HAZARD
AVOIDANCE

2) Use the NOSE UP/NOSE DN Keys or push the CWS Button while hand-flying the aircraft to adjust the
commanded airspeed while maintaining the same power, or reduce power to allow descent in Flight Level
Change Mode while the autopilot maintains the current airspeed.
3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.

AFCS

ADDITIONAL
FEATURES

The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the
autopilot transitions to Altitude Hold Mode and levels the aircraft.

APPENDICES

Cruise Altitude of 12,000 MSL
ALT Mode

2
FLC

Mod

3
Selected Altitude of 10,000 MSL
ALT Mode

INDEX

Figure 7-34 FLC Descent

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SYSTEM
OVERVIEW

Automatic Flight Control System
Vertical Path Tracking descent to VNV Target Altitude:
1) Select VNV flight control:

FLIGHT
INSTRUMENTS

a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears.

b) Using the ALT Knob, set the Selected Altitude below the flight plan’s VNV Target Altitude of 10,000 feet.

EIS

If the Selected Altitude is not at least 75 ft below the VNV Target Altitude, the flight director captures the
Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active (ALTS is
armed rather than ALTV).

AUDIO PANEL
& CNS

c) If Vertical Path Tracking Mode is armed more than 5 minutes prior to descent path capture, acknowledgment is
required for the flight director to transition from Altitude Hold to Vertical Path Tracking Mode. To proceed with
descent path capture if the white ‘VPTH’ annunciation begins flashing, do one of the following

• Press the VNV Key

• Turn the ALT Knob to adjust the Selected Altitude

If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the
descent is not captured.
2) When the top of descent (TOD) is reached, the flight director transitions to Vertical Path Tracking Mode and
begins the descent to the VNV Target Altitude. Intention to capture the VNV Target Altitude is indicated by the
white ‘ALTV’ annunciation.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AFCS

3) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode,
indicated by the green ‘ALTV’ annunciation flashing for up to 10 seconds.

ADDITIONAL
FEATURES

The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude;
the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint.

ALT Mode

TOD

Cruise Altitude of 12,000 MSL

2
VPT

APPENDICES

ode

3
VNAV Target Altitude of 10,000 MSL

BOD

ALT Mode

Selected Altitude (set below VNAV Target Altitude)

INDEX

3 nm

OPSHN

Figure 7-35 VPTH Descent

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SYSTEM
OVERVIEW

Non-path descent using Flight Level Change Mode:
1) Using Flight Level Change Mode, command a non-path descent to an intermediate altitude above the next VNV
flight plan altitude:

FLIGHT
INSTRUMENTS

a) Using the ALT Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case
9,400 feet) at which to level off between VNV flight plan altitudes.
b) Press the FLC Key before the planned TOD during an altitude hold while VPTH is armed. The Airspeed Reference
defaults to the current aircraft airspeed. Vertical Path Tracking and Selected Altitude Capture Mode are armed
automatically.

EIS

2) Reduce power to allow descent in Flight Level Change Mode. The autopilot maintains the Airspeed Reference.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.

The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the
autopilot transitions to Altitude Hold Mode and levels the aircraft. After leveling off, reset Selected Altitude at
or below 9,000 ft.

HAZARD
AVOIDANCE

4) When the next TOD is reached, Vertical Path Tracking becomes active (may require acknowledgment to allow
descent path capture).

AFCS

5) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode,
indicated by the green ‘ALTV’ annunciation flashing for up to 10 seconds.

ADDITIONAL
FEATURES

APPENDICES
INDEX

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EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Automatic Flight Control System

AUDIO PANEL
& CNS

Planned
TOD

BOD

ALT Mode

Pla

Selected Altitude of 9,400 MSL

VNAV Target Altitude of 10,000 MSL

sce

ALT Mode

Pa
th
TOD

FLIGHT
MANAGEMENT

VNAV Target Altitude of 9,000 MSL

BOD

ALT Mode

Selected Altitude

HAZARD
AVOIDANCE

3 nm

OPSHN

HABUK

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 7-36 Non-path Descent

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Automatic Flight Control System
SYSTEM
OVERVIEW

Approach
Flying an ILS approach:

FLIGHT
INSTRUMENTS

1) Transition from GPS Navigation Mode to Heading Select Mode.
a) Select the Runway 35L ILS approach for KCOS and select ‘VECTORS’ for the transition. Load and activate the
approach into the flight plan.
b) Use the HDG Knob to set the Selected Heading after getting vectors from ATC.
c) Press the HDG Key. The autopilot turns the aircraft to the desired heading.

EIS

d) Use Heading Select Mode to comply with ATC vectors as requested.

AUDIO PANEL
& CNS

2) Arm LOC Approach and Glideslope modes.
a) Ensure the appropriate localizer frequency is tuned.
b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear
in white as armed mode annunciations.

FLIGHT
MANAGEMENT

c) The navigation source automatically switches to LOC. After this switch occurs, the localizer signal can be captured
and the flight director determines when to begin the turn to intercept the final approach course. The flight
director now provides guidance to the missed approach point.
• Push the AP DISC Switch at the decision
height and land the aircraft.

HAZARD
AVOIDANCE

3) There are two options available at this point, as the autopilot flies the ILS approach:
• Use the GA Switch to execute a missed
approach.

KCOS

AFCS

LOC APR/
GS Mode

3
PETEY

ADDITIONAL
FEATURES

e
od

PYNON

APPENDICES

GPS NAV Mode

INDEX

Figure 7-37 ILS Approach to KCOS

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SYSTEM
OVERVIEW

Automatic Flight Control System

NOTE: Support for WAAS precision approaches is available only in installations with GIA 63W IAUs when

WAAS is available.

FLIGHT
INSTRUMENTS

Flying a RNAV GPS approach with vertical guidance:
1) Arm flight director modes for a RNAV GPS approach with vertical guidance:
a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source).
b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan.

EIS

2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and
Glidepath Mode is armed.

AUDIO PANEL
& CNS

3) Once the glidepath is captured, Glidepath Mode becomes active. The flight director now provides guidance to
the missed approach point.

FLIGHT
MANAGEMENT

4) There are two options available at this point, as the autopilot flies the approach:
• Push the AP DISC Switch at the Decision
height and land the aircraft.

• Use the GA Switch to execute a missed
approach.

HAZARD
AVOIDANCE

KCOS

AFCS

GPS APR/
GP Mode

CEGIX

2
ADDITIONAL
FEATURES

FALUR

HABUK

INDEX

GPS NAV Mode

APPENDICES

PYNON

Figure 7-38 LPV Approach to KCOS

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SYSTEM
OVERVIEW

Go Around/Missed Approach
Note: As a result of calculations performed by the system while flying the holding pattern, the display may

FLIGHT
INSTRUMENTS

re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and
MFD.
Flying a missed approach:

EIS

1) Push the GA Switch at the Decision Height and apply go around power to execute a missed approach. The
flight director Command Bars establish a nose-up climb to follow. If flying an ILS or LOC approach the CDI also
switches to GPS as the navigation source.

Note that when the GA Switch is pushed, the missed approach is activated and the autopilot disconnects,
indicated by the ‘AP’ annunciation flashing yellow for 5 seconds.

AUDIO PANEL
& CNS

Flashes 5 sec

2) Start the climb to the prescribed altitude in the published Missed Approach Procedure (in this case, 10,000 ft).

FLIGHT
MANAGEMENT

a) Press the AP Key to re-engage the autopilot.
b) Press the NAV Key to have the autopilot fly to the hold.

HAZARD
AVOIDANCE

3) Use the ALT Knob to set a Selected Altitude to hold.
To hold the current airspeed during the climb, press the FLC Key.

ADDITIONAL
FEATURES

AFCS

As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.

The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the
autopilot transitions to Altitude Hold Mode and levels the aircraft.

APPENDICES

4) The autopilot flies the holding pattern after the missed approach is activated. Annunciations are displayed in
the Navigation Status Box, above the AFCS Status Box.

INDEX

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FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Automatic Flight Control System

EIS

FLIGHT
MANAGEMENT

GPS NAV Mode

AUDIO PANEL
& CNS

MOGAL

3
2

HAZARD
AVOIDANCE

GA Mode

KCOS

AFCS

INDEX

APPENDICES

ADDITIONAL
FEATURES

Figure 7-39 Go Around/Missed Approach

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Automatic Flight Control System
SYSTEM
OVERVIEW

7.7 AFCS Annunciations and Alerts
AFCS Status Alerts

FLIGHT
INSTRUMENTS

The annunciations in Table 7-5 (listed in order of increasing priority) can appear on the PFD above the
Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by
criticality.
AFCS Status Annunciation

EIS
AUDIO PANEL
& CNS

Figure 7-40 AFCS Status Annunciation

Aileron Mistrim Right
Aileron Mistrim Left
Elevator Mistrim Down
Pitch Trim Failure
(or stuck AP TRIM
Switch)

Description
Roll servo providing sustained force in the indicated direction

Pitch servo providing sustained force in the indicated direction
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move AP TRIM switches separately to unstick
Roll axis control failure; AP inoperative

Pitch Failure

Pitch axis control failure; AP inoperative
AP and MET are unavailable; FD may still be available

ADDITIONAL
FEATURES

Preflight Test

AFCS

Roll Failure

System Failure

HAZARD
AVOIDANCE

Elevator Mistrim Up

Annunciation

FLIGHT
MANAGEMENT

Alert Condition

APPENDICES

Performing preflight system test; aural alert sounds at completion
Do not press the AP DISC Switch during servo power-up and preflight
system tests as this may cause the preflight system test to fail or never
to start (if servos fail their power-up tests). Power must be cycled to
the servos to remedy the situation.
Preflight system test failed; aural alert sounds at failure
Table 7-5 AFCS Status Field Alerts

INDEX

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SYSTEM
OVERVIEW

Overspeed Protection

FLIGHT
INSTRUMENTS

While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude capture mode is
active, airspeed is monitored by the flight director and pitch commands are limited for overspeed protection.
Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode
reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed.

EIS

Automatic Flight Control System

When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed
Indicator, flashing a yellow ‘MAXSPD’ annunciation. Engine power should be reduced and/or the pitch reference
adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved.

AUDIO PANEL
& CNS

Note: Overspeed protection is not active in Altitude Hold, Glideslope or Glidepath Modes.

FLIGHT
MANAGEMENT

Airspeed
Indicator

Figure 7-41 Overspeed Annunciation

HAZARD
AVOIDANCE

Annunciations for KAP 140 Autopilot System
Note: Refer to the autopilot manufacturer’s Pilot’s Guide for more information.

ADDITIONAL
FEATURES

AFCS

When GPS approach mode becomes active and the necessary approach criteria are met, a message appears
in the AFCS Status Box alerting the pilot to a change in autopilot NAV source (“NAV Source Changed – Select
Desired Autopilot Mode”). The annunciation shall blink for five seconds and remain in the AFCS Status Box
for 30 seconds.

Figure 7-42 KAP 140 Annunciation (Informative)

APPENDICES

NOTE: KAP 140 equipped aircraft only: Each time the CDI Softkey is pressed or the navigation source

INDEX

is changed (i.e. missed approach), the following message appears in the message window, “NAV Source
Changed – Select Desired Autopilot Mode.”

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Additional Features
SYSTEM
OVERVIEW

Section 8 Additional Features

FLIGHT
INSTRUMENTS

NOTE: With the availability of SafeTaxi, ChartView, or FliteCharts in electronic form, it is still advisable to

carry another source of charts on board the aircraft.
Additional features of the system include the following:
• Synthetic Vision System (SVS)
• SafeTaxi® diagrams

EIS

• ChartView and FliteCharts® electronic charts
• XM Radio entertainment

AUDIO PANEL
& CNS

• Scheduler
• Electronic Checklists

FLIGHT
MANAGEMENT

The optional Synthetic Vision System (SVS) provides a three-dimensional forward view of terrain features on
the PFD. SVS imagery shows the pilot’s view of relevant features in relation to the aircraft attitude, as well as the
flight path pertaining to the active flight plan.
SafeTaxi diagrams provide detailed taxiway, runway, and ramp information at more than 700 airports in the
United States. By decreasing range on an airport that has a SafeTaxi diagram available, a close up view of the
airport layout can be seen.

HAZARD
AVOIDANCE

The optional ChartView and FliteCharts provide on-board electronic terminal procedures charts. Electronic
charts offer the convenience of rapid access to essential information. Either ChartView or FliteCharts may be
configured in the system, but not both.

AFCS

The optional XM Radio entertainment audio feature of the GDL 69A Data Link Receiver handles more than 170
channels of music, news, and sports. XM Radio offers more entertainment choices and longer range coverage
than commercial broadcast stations.
The Scheduler feature can be used to enter and display short term or long term reminder messages such as
Switch fuel tanks, Change oil, or Altimeter-Transponder Check in the Messages Window on the PFD.

ADDITIONAL
FEATURES

Optional checklists help to quickly find the proper procedure on the ground or during flight.

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Additional Features

8.1 Synthetic Vision System (SVS) (Optional)

FLIGHT
INSTRUMENTS

WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.

SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability
upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.

AUDIO PANEL
& CNS

EIS

The optional Synthetic Vision System (SVS) is a visual enhancement to the G1000 Integrated Flight Deck. SVS
depicts a forward-looking attitude display of the topography immediately in front of the aircraft. The field of
view is 30 degrees to the left and 35 degrees to the right. SVS information is shown on the Primary Flight Display
(PFD), or on the Multifunction Display (MFD) in Reversionary Mode (Figure 8‑81). The depicted imagery is
derived from the aircraft attitude, heading, GPS three-dimensional position, and a nine arc-second database of
terrain, obstacles, and other relevant features. The terrain data resolution of nine arc-seconds, meaning that
the terrain elevation contours are stored in squares measuring nine arc-seconds on each side, is required for the
operation of SVS. Loss of any of the required data, including temporary loss of the GPS signal, will cause SVS to
be disabled until the required data is restored.

HAZARD
AVOIDANCE

The optional Terrain Awareness and Warning System (TAWS) or standard Terrain-SVS is integrated within
SVS to provide visual and auditory alerts to indicate the presence of terrain and obstacle threats relevant to the
projected flight path. Terrain alerts are displayed in red and yellow shading on the PFD.

AFCS

FLIGHT
MANAGEMENT

The SVS terrain display shows land contours (colors are consistent with those of the topographical map display),
large water features, towers, and other obstacles over 200’ AGL that are included in the obstacle database. Cultural
features on the ground such as roads, highways, railroad tracks, cities, and state boundaries are not displayed
even if those features are found on the MFD map. The terrain display also includes a north–south east–west grid
with lines oriented with true north and spaced at one arc-minute intervals to assist in orientation relative to the
terrain.

The terrain display is intended for situational awareness only. It may not provide the accuracy or fidelity on
which to base decisions and plan maneuvers to avoid terrain or obstacles. Navigation must not be predicated
solely upon the use of the Terrain–SVS or TAWS terrain or obstacle data displayed by the SVS.
• Pathways

• Airport Signs

• Flight Path Marker

• Runway Display

• Horizon Heading Marks

• Terrain Alerting

• Traffic Display

• Obstacle Alerting

INDEX

APPENDICES

ADDITIONAL
FEATURES

The following SVS enhancements appear on the PFD:

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-1 Synthetic Vision Imagery

SVS Operation

HAZARD
AVOIDANCE

SVS is activated from the PFD using the softkeys located along the bottom edge of the display. Pressing the
softkeys turns the related function on or off. When SVS is enabled, the pitch scale increments are reduced to
10 degrees up and 7.5 degrees down.

AFCS

SVS functions are displayed on three levels of softkeys. The PFD Softkey leads into the PFD function Softkeys,
including synthetic vision. Pressing the SYN VIS Softkey displays the SVS feature softkeys. The softkeys are
labeled PATHWAY, SYN TERR, HRZN HDG, and APTSIGNS. The BACK Softkey returns to the previous
level of softkeys. Synthetic Terrain must be active before any other SVS feature may be activated.

ADDITIONAL
FEATURES

HRZN HDG, APTSIGNS, and PATHWAY Softkeys are only available when the SYN TERR Softkey is
activated (gray with black characters). After activating the SYN TERR Softkey, the HRZN HDG, APTSIGNS,
and PATHWAY softkeys may be activated in any combination to display desired features. When system power
is cycled, the last selected state (on or off) of the SYN TERR, HRZN HDG, APTSIGNS, and PATHWAY
softkeys is remembered by the system.

APPENDICES

• PATHWAY Softkey enables display of rectangular boxes that represent course guidance.
• SYN TERR Softkey enables synthetic terrain depiction.
• HRZN HDG Softkey enables horizon heading marks and digits.
• APTSIGNS Softkey enables airport signposts.

INDEX

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SYSTEM
OVERVIEW

Additional Features

FLIGHT
INSTRUMENTS

PFD

SYN VIS

BACK

Pressing the BACK Softkey
returns to the top-level softkeys.

BACK

EIS

PATHWAY SYN TERR HRZN HDG APTSIGNS

AUDIO PANEL
& CNS

Pressing the BACK Softkey returns to the previous level of softkeys.

Figure 8-2 SVS Softkeys

Activating and deactivating SVS:

FLIGHT
MANAGEMENT

1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the SYN TERR Softkey. The SVS display will cycle on or off with the SYN TERR Softkey.

HAZARD
AVOIDANCE

Activating and deactivating Pathways:
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the PATHWAY Softkey. The Pathway feature will cycle on or off with the PATHWAY Softkey.

AFCS

Activating and deactivating Horizon Headings:
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.

ADDITIONAL
FEATURES

3) Press the HRZN HDG Softkey. The horizon heading display will cycle on or off with the HRZN HDG Softkey.

Activating and deactivating Airport Signs:
1) Press the PFD Softkey.

APPENDICES

2) Press the SYN VIS Softkey.

INDEX

3) Press the APTSIGNS Softkey. Display of airport signs will cycle on or off with the APTSIGNS Softkey.

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Additional Features
SYSTEM
OVERVIEW

SVS Features

FLIGHT
INSTRUMENTS

Selected
Altitude

Airport
Runway

Pathways
Color
Matches CDI
Indicating
NAV Source

Flight
Path
Marker
Airplane
Symbol

EIS

Zero
Pitch Line
(ZPL) with
Compass
Heading
Marks

AUDIO PANEL
& CNS

Synthetic
Terrain

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

SVS
Softkeys
Figure 8-3 SVS on the Primary Flight Display

NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation

information provided by the CDI, VSI, and VDI.
AFCS

Pathways

ADDITIONAL
FEATURES

Pathways provide a three-dimensional perspective view of the selected route of flight shown as colored
rectangular boxes representing the horizontal and vertical flight path of the active flight plan. The box
size represents 700 feet wide by 200 feet tall during enroute, oceanic, and terminal flight phases. During
an approach, the box width is 700 feet or one half full scale deviation on the HSI, whichever is less. The
height is 200 feet or one half full scale deviation on the VDI, whichever is less. The altitude at which the
pathway boxes are displayed is determined by the higher of either the selected altitude or the VNAV altitude
programmed for the active leg in the flight plan (Figure 8-4).

APPENDICES

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INDEX

The color of the rectangular boxes may be magenta, green, or white depending on the route of flight and
navigation source selected. The active GPS or GPS overlay flight plan leg is represented by magenta boxes
that correspond to the Magenta CDI. A localizer course is represented by green boxes that correspond to a
green CDI. An inactive leg of an active flight plan is represented by white boxes corresponding to a white line
drawn on the Inset map or MFD map indicating an inactive leg.

407

SYSTEM
OVERVIEW

Additional Features

FLIGHT
INSTRUMENTS

Selected
Altitude

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Programmed
Altitudes

HAZARD
AVOIDANCE

Figure 8-4 Programmed and Selected Altitude

AFCS

Pathways provide supplemental glidepath information on an active ILS, LPV, LNAV/VNAV, and some LNAV
approaches. Pathways are intended as an aid to situational awareness and should not be used independent
of the CDI, VDI, glide path indicator, and glide slope indicator. They are removed from the display when
the selected navigation information is not available. Pathways are not displayed beyond the active leg when
leg sequencing is suspended and are not displayed on any portion of the flight plan leg that would lead to
intercepting a leg in the wrong direction.

Departure and Enroute

APPENDICES

ADDITIONAL
FEATURES

Prior to intercepting an active flight plan leg, pathways are displayed as a series of boxes with pointers at
each corner that point in the direction of the active waypoint. Pathways are not displayed for the first leg
of the flight plan if that segment is a Heading-to-Altitude leg. The first segment displaying pathways is the
first active GPS leg or active leg with a GPS overlay. If this leg of the flight plan route is outside the SVS
field of view, pathways will not be visible until the aircraft has turned toward this leg. While approaching
the center of the active leg and prescribed altitude, the number of pathway boxes decreases to a minimum
of four.

INDEX

Pathways are displayed along the flight plan route at the highest of either the selected altitude or the
programmed altitude for the leg. Climb profiles cannot be displayed due to the variables associated with
aircraft performance. Flight plan legs requiring a climb are indicated by pathways displayed at a level above
the aircraft at the altitude selected or programmed.

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Additional Features
SYSTEM
OVERVIEW

Descent and Approach

FLIGHT
INSTRUMENTS

Pathways are shown descending only for a programmed descent (Figures 8-5, 8-6). When the flight plan
includes programmed descent segments, pathways are displayed along the descent path provided that the
selected altitude is lower than the programmed altitude.

EIS

During a Vectors-to-Final (VTF) approach transition, pathways are displayed along the final approach
course inbound to the Missed Approach Point (MAP). Pathways are shown level at the selected altitude
or at the next programmed crossing altitude, whichever is higher, up to the point along the final approach
course where the altitude intercepts the extended vertical descent path, glidepath, or glideslope. From
the vertical path descent, glidepath, or glideslope intercept point, the pathways are shown inbound to the
Missed Approach Point (MAP) along the published lateral and vertical descent path.

AUDIO PANEL
& CNS

During an ILS approach, the initial approach segment is displayed in magenta at the segment altitudes
if GPS is selected as the navigation source on the CDI. When switching to localizer inbound with LOC
selected as the navigation source on the CDI, pathways are displayed in green along the localizer and glide
slope.

FLIGHT
MANAGEMENT

VOR, LOC BC, and ADF approach segments that are approved to be flown using GPS are displayed in
magenta boxes. Segments that are flown using other than GPS or ILS, such as heading legs or VOR final
approach courses are not displayed.
Selected Altitude
set for Enroute
Selected Altitude
set for Departure

HAZARD
AVOIDANCE

Climbs NOT
displayed
by pathway

Non-programmed descents NOT displayed by pathway

TOD

AFCS

Selected Altitude
for Step Down

Programmed descent
displayed by pathway

ADDITIONAL
FEATURES
APPENDICES

Selected Altitude or Programmed Altitude
(whichever is higher)

Figure 8-5 SVS Pathways, Enroute and Descent

INDEX

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SYSTEM
OVERVIEW

Additional Features
Missed Approach

FLIGHT
INSTRUMENTS

Upon activating the missed approach, pathways lead to the Missed Approach Holding Point (MAHP) and
are displayed as a level path at the published altitude for the MAHP, or the selected altitude, whichever is
the highest. If the initial missed approach leg is a Course-to-Altitude (CA) leg, the pathways boxes will
be displayed level at the altitude published for the MAHP. If the initial missed approach leg is defined by
a course using other than GPS, pathways are not displayed for that segment. In this case, the pathways
displayed for the next leg may be outside the field of view and will be visible when the aircraft has turned
in the direction of that leg.

AUDIO PANEL
& CNS

EIS

Pathways are displayed along each segment including the path required to track course reversals that are
part of a procedure, such as holding patterns. Pathways boxes will not indicate a turn to a MAHP unless a
defined geographical waypoint exists between the MAP and MAHP.

FAF

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Descent displayed
by pathway

Selected Altitude
or Programmed Altitude
(whichever is higher)

MAP Climbs NOT displayed
by pathway

Turn Segment
NOT displayed
by pathway

APPENDICES

ADDITIONAL
FEATURES

AFCS

MAHP

INDEX

Figure 8-6 SVS Pathways, Approach, Missed Approach, and Holding

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Additional Features
SYSTEM
OVERVIEW

Flight Path Marker

FLIGHT
INSTRUMENTS

The Flight Path Marker (FPM), also known as a Velocity Vector, is displayed on the PFD at groundspeeds
above 30 knots. The FPM depicts the approximate projected path of the aircraft accounting for wind speed
and direction relative to the three-dimensional terrain display.
The FPM is always available when the Synthetic Terrain feature is in operation. The FPM represents the
direction of the flight path as it relates to the terrain and obstacles on the display, while the airplane symbol
represents the aircraft heading.

EIS

The FPM works in conjunction with the Pathways feature to assist the pilot in maintaining desired altitudes
and direction when navigating a flight plan. When on course and altitude the FPM is aligned inside the
pathway boxes as shown (Figure 8-7).

AUDIO PANEL
& CNS

The FPM may also be used to identify a possible conflict with the aircraft flight path and distant terrain or
obstacles. Displayed terrain or obstacles in the aircraft’s flight path extending above the FPM could indicate
a potential conflict, even before an alert is issued by TAWS. However, decisions regarding terrain and/or
obstacle avoidance should not be made using only the FPM.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Flight Path
Marker
(FPM)

AFCS

Wind
Vector

ADDITIONAL
FEATURES
APPENDICES

Figure 8-7 Flight Path Marker and Pathways

Zero Pitch Line

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INDEX

The Zero Pitch Line is drawn completely across the display and represents the aircraft attitude with respect
to the horizon. It may not align with the terrain horizon, particularly when the terrain is mountainous or
when the aircraft is flown at high altitudes.

411

SYSTEM
OVERVIEW

Additional Features
Horizon Heading

FLIGHT
INSTRUMENTS

The Horizon Heading is synchronized with the HSI and shows approximately 60 degrees of compass
heading in 30‑degree increments on the Zero Pitch Line. Horizon Heading tick marks and digits appearing
on the zero pitch line are not visible behind either the airspeed or altitude display. Horizon Heading is used
for general heading awareness, and is activated and deactivated by pressing the HRZN HDG Softkey.

Traffic
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the SVS display or may appear as a

EIS

partial symbol.

AUDIO PANEL
& CNS

Traffic symbols are displayed in their approximate locations as determined by the related traffic systems.
Traffic symbols are displayed in three dimensions, appearing larger as they are getting closer, and smaller
when they are further away. Traffic within 1000 feet laterally of the aircraft will not be displayed on the SVS
display. Traffic symbols and coloring are consistent with that used for traffic displayed in the Inset map or
MFD traffic page. If the traffic altitude is unknown, the traffic will not be displayed on the SVS display. For
more details refer to the traffic system discussion in the Hazard Avoidance section.

FLIGHT
MANAGEMENT

Airport Signs

HAZARD
AVOIDANCE

Airport Signs provide a visual representation of airport location and identification on the synthetic terrain
display. When activated, the signs appear on the display when the aircraft is approximately 15 nm from
an airport and disappear at approximately 4.5 nm. Airport signs are shown without the identifier until
the aircraft is approximately eight nautical miles from the airport. Airport signs are not shown behind the
airspeed or altitude display. Airport signs are activated and deactivated by pressing the APTSIGNS Softkey.

AFCS

Traffic

Airport
Sign
without
Identifier
(Between
8 nm and
15 nm)

INDEX

APPENDICES

ADDITIONAL
FEATURES

Airport
Sign with
Identifier
(Between
4.5 nm and
8 nm)

Figure 8-8 Airport Signs

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Additional Features
SYSTEM
OVERVIEW

Runways
WARNING: Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft

FLIGHT
INSTRUMENTS

to the runway or for maintaining the proper approach path angle during landing.

EIS

Runway data provides improved awareness of runway location with respect to the surrounding terrain. All
runway thresholds are depicted at their respective elevations as defined in the database. In some situations,
where threshold elevations differ significantly, crossing runways may appear to be layered. As runways are
displayed, those within 45 degrees of the aircraft heading are displayed in white. Other runways will be gray
in color. When an approach for a specific runway is active, that runway will appear brighter and be outlined
with a white box, regardless of the runway orientation as related to aircraft heading. As the aircraft gets closer
to the runway, more detail such as runway numbers and centerlines will be displayed.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Runway
Selected for
Approach

Other
Runway
on Airport

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Figure 8-9 Airport Runways

APPENDICES
INDEX

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413

SYSTEM
OVERVIEW

Additional Features
Terrain-SVS and TAWS Alerting

FLIGHT
INSTRUMENTS

Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA)
alerts, and corresponds to the red and yellow X symbols on the Inset Map and MFD map displays. For more
detailed information regarding Terrain-SVS and TAWS, refer to the Hazard Avoidance Section.

EIS

In some instances, a terrain or obstacle alert may be issued with no conflict shading displayed on the
synthetic terrain. In these cases, the conflict is outside the SVS field of view to the left or right of the
aircraft.

AUDIO PANEL
& CNS

TERRAIN
Annunciation

FLIGHT
MANAGEMENT

Terrain
Caution

HAZARD
AVOIDANCE

Potential
Impact
Point

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 8-10 Terrain Alert

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

Obstacles are represented on the synthetic terrain display by standard two-dimensional tower symbols found
on the Inset map and MFD maps and charts. Obstacle symbols appear in the perspective view with relative
height above terrain and distance from the aircraft. Unlike the Inset map and MFD moving map display,
obstacles on the synthetic terrain display do not change colors to warn of potential conflict with the aircraft’s
flight path until the obstacle is associated with an actual FLTA alert. Obstacles greater than 1000 feet below the
aircraft altitude are not shown. Obstacles are shown behind the airspeed and altitude displays.

EIS

TERRAIN
Annunciation

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Obstacle
Warning

HAZARD
AVOIDANCE

Potential
Impact
Point

Figure 8-11 Obstacle
AFCS

Field of View
ADDITIONAL
FEATURES

The PFD field of view can be represented on the MFD Navigation Map Page. Two dashed lines forming a
V‑shape in front of the aircraft symbol on the map, represent the forward viewing area shown on the PFD.
Configuring field of view:

APPENDICES

1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key.

INDEX

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EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Additional Features

AUDIO PANEL
& CNS

Field of
View

FLIGHT
MANAGEMENT

Navigation Map Page OPTIONS Menu

Map Setup Menu, Map Group, Field of View Option

Figure 8-12 Option Menus

3) Turn the FMS Knob to select the Map Group and press the ENT Key.

HAZARD
AVOIDANCE

4) Turn the large FMS Knob to scroll through the Map Group options to FIELD OF VIEW.
5) Turn the small FMS Knob to select On or Off.
6) Press the FMS Knob to return to the Navigation Map Page.

ADDITIONAL
FEATURES

AFCS

The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF
VIEW turned on.

APPENDICES

Lines
Depict
PFD Field
of View

INDEX

SVS View on the PFD

Field of View on the MFD

Figure 8-13 PFD and MFD Field of View Comparison

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Additional Features
SYSTEM
OVERVIEW

8.2 SafeTaxi

FLIGHT
INSTRUMENTS

SafeTaxi is an enhanced feature that gives greater map detail when viewing airports at close range. The
maximum map ranges for enhanced detail are pilot configurable. When viewing at ranges close enough to
show the airport detail, the map reveals taxiways with identifying letters/numbers, airport Hot Spots, and airport
landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at
lower map ranges. When the MFD display is within the SafeTaxi ranges, the airplane symbol on the airport
provides enhanced position awareness.

EIS

Designated Hot Spots are recognized at airports with many intersecting taxiways and runways, and/or complex
ramp areas. Airport Hot Spots are outlined to caution pilots of areas on an airport surface where positional
awareness confusion or runway incursions happen most often. Hot Spots are defined with a magenta circle or
outline around the region of possible confusion.

• VOR Information Page

• Inset Map (PFD)

• User Waypoint Information Page

• Weather Datalink Page

• Trip Planning Page

• Airport Information Page

• Nearest Pages

• Intersection Information Page

• Active and Stored Flight Plan Pages

FLIGHT
MANAGEMENT

• Navigation Map Page

AUDIO PANEL
& CNS

Any map page that displays the navigation view can also show the SafeTaxi airport layout within the maximum
configured range. The following is a list of pages where the SafeTaxi feature can be seen:

HAZARD
AVOIDANCE

• NDB Information Page
During ground operations the aircraft’s position is displayed in reference to taxiways, runways, and airport
features. In the example shown, the aircraft is on taxiway Bravo inside the High Alert Intersection boundary
on KSFO airport. Airport Hot Spots are outlined in magenta. When panning over the airport, features such as
runway holding lines and taxiways are shown at the cursor.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Additional Features

Taxiway
Identification

EIS

Aircraft
Position

AUDIO PANEL
& CNS

Airport Hot
Spot Outline

FLIGHT
MANAGEMENT

Airport
Features

Figure 8-14 SafeTaxi Depiction on the Navigation Map Page

DCLTR Softkey
Removes Taxiway
Markings

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

The DCLTR Softkey (declutter) label advances to DCLTR-1, DCLTR -2, and DCLTR-3 each time the softkey is
pressed for easy recognition of decluttering level. Pressing the DCLTR Softkey removes the taxiway markings
and airport feature labels. Pressing the DCLTR-1 Softkey removes VOR and station ID, the VOR symbol, and
intersection names if within the airport plan view. Pressing the DCLTR-2 Softkey removes the airport runway
layout, unless the airport in view is part of an active route structure. Pressing the DCLTR-3 Softkey cycles back
to the original map detail. Refer to Map Declutter Levels in the Flight Management Section.

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Additional Features
SYSTEM
OVERVIEW

Configuring SafeTaxi range:
1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

Figure 8-15 Navigation Map PAGE MENU, Map Setup Option

3) Turn the FMS Knob to select the Aviation Group and press the ENT Key.
4) Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI.

FLIGHT
MANAGEMENT

5) Turn the small FMS Knob to display the range of distances.
6) Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range.
7) Press the ENT Key to complete the selection.

HAZARD
AVOIDANCE

8) Press the FMS Knob to return to the Navigation Map Page.

AFCS

SAFETAXI
Option

ADDITIONAL
FEATURES

SafeTaxi
Range
Options

APPENDICES
INDEX

Figure 8-16 MAP SETUP Menu, Aviation Group, SAFETAXI Range Options

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SYSTEM
OVERVIEW

Additional Features

SafeTaxi Cycle Number and Revision

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

The SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date.
When turning on the G1000, the Power-up Page indicates whether the databases are current, out of date, or not
available. The Power-up Page shows the SafeTaxi database is current when the SafeTaxi Expires date is shown in
white. When the SafeTaxi cycle has expired, the SafeTaxi Expires date appears in yellow. The message SafeTaxi:
N/A appears in white if no SafeTaxi data is available on the database card.

SafeTaxi Database has Expired

APPENDICES

ADDITIONAL
FEATURES

AFCS

SafeTaxi Database is Current

INDEX

SafeTaxi Database Not Available
Figure 8-17 Power-up Page, SafeTaxi Database

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found
on the AUX - System Status page. SafeTaxi information appears in blue and yellow text. The EFFECTIVE
date appears in blue when data is current and in yellow when the current date is before the effective date.
The EXPIRES date appears in blue when data is current and in yellow when expired (Figures 8‑18 and 8-19).
SafeTaxi REGION NOT AVAILABLE appears in blue if SafeTaxi data is not available on the database card
(Figure 8‑19). Expired SafeTaxi data is never disabled.
Press the DBASE Softkey for scrolling through the database information. Scroll through the database with
the FMS knob or ENT Key.
The SafeTaxi database cycle number shown in the figure, 08S6, is deciphered as follows:

EIS

08 – Indicates the year 2008
S – Indicates the data is for SafeTaxi

AUDIO PANEL
& CNS

6 – Indicates the sixth issue of the SafeTaxi database for the year
The SafeTaxi EFFECTIVE date 25–OCT–08 is the beginning date for the current database cycle. SafeTaxi
EXPIRES date 20–DEC–08 is the revision date for the next database cycle.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

SafeTaxi Data

ADDITIONAL
FEATURES

Figure 8-18 AUX – System Status Page, SafeTaxi Current Information
APPENDICES

The SafeTaxi database is provided by Garmin. Refer to Updating Garmin Databases in Appendix B for
instructions on revising the SafeTaxi database.

INDEX

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SYSTEM
OVERVIEW

Additional Features

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

The other three possible AUX - System Status page conditions are shown here. The EFFECTIVE date is the
beginning date for this database cycle. If the present date is before the effective date, the EFFECTIVE date
appears in yellow and the EXPIRES date appears in blue. The EXPIRES date is the revision date for the next
database cycle. NOT AVAILABLE indicates that SafeTaxi is not available on the database card or no database
card is inserted.

SafeTaxi Database has Expired

APPENDICES

ADDITIONAL
FEATURES

AFCS

Current Date is before Effective Date

INDEX

SafeTaxi Database Not Installed
Figure 8-19 AUX – System Status Page, SafeTaxi Expired, SafeTaxi Not Available

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Additional Features
SYSTEM
OVERVIEW

8.3 ChartView

FLIGHT
INSTRUMENTS

ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full
color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the plan view
of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta.
The ChartView database subscription is available from Jeppesen, Inc. Available data includes:
• Arrivals (STAR)
• Airport Diagrams
• Departure Procedures (DP)

• NOTAMs
EIS

• Approaches

ChartView Softkeys
AUDIO PANEL
& CNS

ChartView functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest
Airports Page, or Flight Plan Page, pressing the SHW CHRT Softkey displays the available terminal chart and
advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO, DP, STAR, APR, WX, NOTAM,
and GO BACK. The chart selection softkeys shown below appear on the Airport Information Page.

FLIGHT
MANAGEMENT

Pressing the GO BACK Softkey reverts to the top level softkeys and previous page.
Pressing the CHRT OPT Softkey advances to the next level of softkeys: ALL, HEADER, PLAN, PROFILE,
MINIMUMS, FIT WDTH, FULL SCN, and BACK.
While viewing the CHRT OPT Softkeys, after 45 seconds of softkey inactivity, the system reverts to the chart
selection softkeys.

HAZARD
AVOIDANCE

SHW CHRT

CHRT

INFO

STAR

APR

NOTAM

GO BACK

AFCS

CHRT OPT

Pressing the GO BACK Softkey returns
to the top-level softkeys and previous page.

HEADER

PLAN

PROFILE

MINIMUMS FIT WDTH FULL SCN

ADDITIONAL
FEATURES

ALL

BACK

Pressing the BACK Softkey returns
to the Chart Selection Softkeys.

APPENDICES

Figure 8-20 ChartView SHW CHRT, Chart Selection, and Chart Option Softkeys

INDEX

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SYSTEM
OVERVIEW

Additional Features

Terminal Procedures Charts
Selecting Terminal Procedures Charts:

FLIGHT
INSTRUMENTS

While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press the SHW CHRT
Softkey.

Or:

1) Press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

3) Press the ENT Key to display the chart.

Navigation Map Page OPTIONS Menu

Waypoint Airport Information Page OPTIONS Menu

Figure 8-21 Option Menus

ADDITIONAL
FEATURES

AFCS

When no terminal procedure chart is available for the nearest airport or the selected airport, the banner
CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to
the Jeppesen subscription, but rather the availability of a particular airport chart selection or procedure for a
selected airport.

APPENDICES

Figure 8-22 Chart Not Available Banner

INDEX

If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner
UNABLE TO DISPLAY CHART is then displayed.

Figure 8-23 Unable To Display Chart Banner

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Additional Features
SYSTEM
OVERVIEW

When a chart is not available by pressing the SHW CHRT Softkey or selecting a Page Menu Option, charts
may be obtained for other airports from the WPT Pages or Flight Plan Pages.

FLIGHT
INSTRUMENTS

If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart
appears on the screen. When no flight plan is active, or when not flying to a direct-to destination, pressing the
SHW CHRT Softkey displays the chart for the nearest airport, if available.
The chart shown is one associated with the WPT – Airport Information page. Usually this is the airport runway
diagram. Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that
page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown.

EIS

Selecting a chart:
1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, press the SHW CHRT
Softkey. The airport diagram or approach chart is displayed on the Airport Information Page.

AUDIO PANEL
& CNS

2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Press the APR Softkey
if the Approach Box is not currently shown).
4) Turn the small and large FMS Knob to enter the desired airport identifier.

FLIGHT
MANAGEMENT

5) Press the ENT Key to complete the airport selection.
6) Turn the large FMS Knob to select the Approach Box.
7) Turn the small FMS Knob to show the approach chart selection choices.

HAZARD
AVOIDANCE

8) Turn either FMS Knob to scroll through the available charts.
9) Press the ENT Key to complete the chart selection.

AFCS

Chart Scale
Select Desired
Approach Chart
From Menu

ADDITIONAL
FEATURES

Scroll Through
Chart With
the Joystick

APPENDICES
INDEX

Figure 8-24 Approach Information Page, Chart Selection

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SYSTEM
OVERVIEW

Additional Features
While the APPROACH Box is selected using the FMS Knob, the G1000 softkeys are blank. Once the desired
chart is selected, the chart scale can be changed and the chart page can be scrolled using the Joystick. Pressing
the Joystick centers the chart on the screen.

FLIGHT
INSTRUMENTS

The aircraft symbol is shown on the chart only if the chart is to scale and the aircraft position is within
the boundaries of the chart. The aircraft symbol is not displayed when the Aircraft Not Shown Icon appears
(Figure 8‑15). If the Chart Scale Box displays a banner NOT TO SCALE, the aircraft symbol is not shown. The
Aircraft Not Shown Icon may appear at certain times, even if the chart is displayed to scale.

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Pressing the CHRT Softkey switches between the ChartView diagram and the associated map in the WPT
page group. In the example shown, the CHRT Softkey switches between the Colorado Springs, CO (KCOS)
Airport Diagram and the navigation map on the WPT – Airport Information page.

INDEX

APPENDICES

ADDITIONAL
FEATURES

Press CHRT Softkey
to Switch Between
ChartView and WPT Airport Information Page

Figure 8-25 CHRT Softkey, Airport Information Page

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Additional Features
SYSTEM
OVERVIEW

Pressing the INFO Softkey returns to the airport diagram when the view is on a different chart. If the
displayed chart is the airport diagram, the INFO Softkey has no effect.

FLIGHT
INSTRUMENTS

The aircraft position is shown in magenta on the ChartView diagrams when the location of the aircraft is
within the chart boundaries. In the example shown, the aircraft is taxiing on Taxiway Alpha on the Charlotte,
NC (KCLT) airport.

EIS

Another source for additional airport information is from the INFO Box above the chart for certain airports.
This information source is not related to the INFO Softkey. When the INFO Box is selected using the FMS
Knob, the G1000 softkeys are blank. The Charlotte, NC airport has five additional charts offering information;
the Airport Diagram, Take-off Minimums, Class B Airspace, Airline Parking Gate Coordinates, and Airline
Parking Gate Location. (The numbers in parentheses after the chart name are Jeppesen designators.)

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Aircraft
Current
Position

HAZARD
AVOIDANCE
AFCS

Figure 8-26 Airport Information Page, INFO View, Full Screen Width
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Additional Features

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

In the example shown in Figure 8-26, the Class B Chart is selected. Pressing the ENT Key displays the
Charlotte Class B Airspace Chart (Figure 8-27).

HAZARD
AVOIDANCE

Figure 8-27 Airport Information Page, Class B Chart Selected from INFO View

Pressing the DP Softkey displays the Departure Procedure Chart if available.

APPENDICES

ADDITIONAL
FEATURES

AFCS

Chart Not
To Scale

INDEX

Aircraft Not
Shown Icon
Figure 8-28 Departure Information Page

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Additional Features
SYSTEM
OVERVIEW

Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available.

FLIGHT
INSTRUMENTS

Chart Not
To Scale

EIS

Change Range
and Scroll
Through the
Chart With the
Joystick

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Aircraft Not
Shown Icon

Figure 8-29 Arrival Information Page

HAZARD
AVOIDANCE

Pressing the APR Softkey displays the approach chart for the airport if available.

AFCS
ADDITIONAL
FEATURES
APPENDICES

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INDEX

Figure 8-30 Approach Information Page

429

SYSTEM
OVERVIEW

Additional Features

EIS

FLIGHT
INSTRUMENTS

Pressing the WX Softkey shows the airport weather frequency information, and includes weather data such as
METAR and TAF from the XM Data Link Receiver, when available. Weather information is available only when
an XM Data Link Receiver is installed and the XM Weather subscription is current.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

WX Info
When
Available

WX Softkey
Selected

HAZARD
AVOIDANCE

Figure 8-31 Weather Information Page

NOTE: A subdued softkey label indicates the function is disabled.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Recent NOTAMS applicable to the current ChartView cycle are included in the ChartView database. Pressing
the NOTAM Softkey shows the local NOTAM information for selected airports, when available. When NOTAMS
are not available, the NOTAM Softkey label appears subdued and is disabled as shown in Figure 8-31. The
NOTAM Softkey may appear on the Airport Information Page and all of the chart page selections.

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

NOTAM
Softkey
Appears for
Selected
Airports
Figure 8-32 NOTAM Softkey Highlighted

HAZARD
AVOIDANCE

Local
NOTAM on
This Airport

AFCS
ADDITIONAL
FEATURES
APPENDICES

NOTAM
Softkey
Selected
Figure 8-33 Airport Information Page, Local NOTAMs

INDEX

Pressing the NOTAM Softkey again removes the NOTAMS information.
Pressing the GO BACK Softkey reverts to the previous page (Navigation Map Page, Nearest Pages, or Flight
Plan Page).
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SYSTEM
OVERVIEW

Additional Features

Chart Options
Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-20).

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Pressing the ALL Softkey shows the complete approach chart on the screen.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Complete
Chart
Shown

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 8-34 Approach Information Page, ALL View

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Additional Features
SYSTEM
OVERVIEW

Pressing the HEADER Softkey shows the header view (approach chart briefing strip) on the screen.

FLIGHT
INSTRUMENTS
EIS

Approach
Chart
Briefing Strip

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-35 Approach Information Page, Header View

HAZARD
AVOIDANCE

Pressing the PLAN Softkey shows the approach chart two dimensional plan view.

AFCS
ADDITIONAL
FEATURES

Approach
Chart Plan
View

APPENDICES
INDEX

Figure 8-36 Approach Information Page, Plan View

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433

SYSTEM
OVERVIEW

Additional Features

EIS

FLIGHT
INSTRUMENTS

Pressing the PROFILE Softkey displays the approach chart descent profile strip.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Approach
Chart Descent
Profile Strip

Figure 8-37 Approach Information Page, Profile View, Full Screen Width

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Pressing the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the
approach chart.

INDEX

APPENDICES

Minimum
Descent
Altitude/
Visibility Strip

Figure 8-38 Approach Information Page, Minimums View, Full Screen Width

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Additional Features
SYSTEM
OVERVIEW

If the chart scale has been adjusted to view a small area of the chart, pressing the FIT WIDTH Softkey
changes the chart size to fit the available screen width.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Press FIT WDTH
Softkey to Show
Full Chart Width
Figure 8-39 Airport Information Page, FIT WDTH Softkey Selected

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Additional Features
Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right.
Selecting Additional Information:

FLIGHT
INSTRUMENTS

1) While viewing the Airport Taxi Diagram, press the FULL SCN Softkey to display the information windows
(AIRPORT, INFO).
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the AIRPORT, INFO, RUNWAYS, or FREQUENCIES Box (INFO Box shown).

EIS

4) Turn the small FMS Knob to select the INFO Box choices. If multiple choices are available, scroll to the desired
choice with the large FMS Knob and press the ENT Key to complete the selection.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

5) Press the FMS Knob again to deactivate the cursor.

AFCS

HAZARD
AVOIDANCE

Available
Information

APPENDICES

ADDITIONAL
FEATURES

Press FULL SCN
Softkey to Switch
Between Full
Screen and Chart
With Info Window

INDEX

Figure 8-40 Airport Information Page, Full Screen and Info Window

Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys.

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Additional Features
SYSTEM
OVERVIEW

The full screen view can also be selected by using the page menu option.
Selecting full screen On or Off:

FLIGHT
INSTRUMENTS

1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.
3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options.
4) Turn the small FMS Knob to choose between the On and Off Full Screen Options.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Chart Setup Option

Full Screen On/Off Selection

HAZARD
AVOIDANCE

Figure 8-41 Page Menus

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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437

SYSTEM
OVERVIEW

Additional Features

Day/Night View

FLIGHT
INSTRUMENTS

ChartView can be displayed on a white or black background for day or night viewing. The Day View offers
a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark
environment. When the CHART SETUP Box is selected the G1000 softkeys are blank.
Selecting Day, Night, or Automatic View:
1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.

HAZARD
AVOIDANCE

Figure 8-42 Waypoint Information Page, OPTIONS Menu

3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑43).
4) Turn the small FMS Knob to choose between Day, Auto, and Night Options.

AFCS

5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to
change the percentage value. The percentage value is the day/night crossover point based on the percentage of
backlighting intensity. For example, if the value is set to 15%, the day/night display changes when the display
backlight reaches 15% of full brightness.

ADDITIONAL
FEATURES

The display must be changed in order for the new setting to become active. This may be accomplished by
selecting another page or changing the display range.

INDEX

APPENDICES

6) Press the FMS Knob when finished to remove the Chart Setup Menu.

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-43 Arrival Information Page, Day View

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 8-44 Arrival Information Page, Night View

INDEX

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

439

SYSTEM
OVERVIEW

Additional Features

ChartView Cycle Number and Expiration Date

FLIGHT
INSTRUMENTS

The ChartView database is revised every 14 days. Charts are still viewable during a period that extends from
the cycle expiration date to the disabled date. ChartView is disabled 70 days after the expiration date and is no
longer available for viewing upon reaching the disabled date. When turning on the G1000, the Power-up Page
indicates any of nine different possible criteria for ChartView availability. See the table below for the various
ChartView Power-up Page displays and the definition of each.

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Power-up Page Display

Definition
Blank Line. G1000 system is not configured for ChartView. Contact
a Garmin-authorized service center for configuration.
System is configured for ChartView but no chart database is
installed. Contact Jeppesen for a ChartView database.
Normal operation. ChartView database is valid and within current
cycle.
ChartView database is within 1 week after expiration date. A new
cycle is available for update.
ChartView database is beyond 1 week after expiration date, but still
within the 70 day viewing period.
ChartView database has timed out. Database is beyond 70 days
after expiration date. ChartView database is no longer available for
viewing.
System time is not available. GPS satellite data is unknown or
G1000 has not yet locked onto satellites. Check database cycle
number for effectivity.
System is verifying chart database when new cycle is installed for the
first time.
After verifying, chart database is found to be corrupt. ChartView is
not available.

ADDITIONAL
FEATURES

Table 8-1 ChartView Power-up Page Annunciations and Definitions

INDEX

APPENDICES

Examples of four possible Power-up Page conditions are shown here. ‘ChartView Disables’ plus a date in
white, indicates chart data is current. This indication for normal operation shows how long the charts may be
viewed. ‘Chart data update available.’ in white, indicates the chart data cycle has expired within the past week
and the next chart cycle is available. ‘Chart data is out of date!’ in yellow, indicates charts are still viewable, but
approaching the disable date. ‘Chart data is disabled.’ in yellow, indicates the chart cycle has been disabled and
is no longer viewable.

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS

Chart Cycle is No
Longer Viewable

HAZARD
AVOIDANCE

Chart Cycle has Expired but is Still Viewable
for 70 Days from Expiration Date

FLIGHT
MANAGEMENT

Chart Cycle has Expired,
Next Cycle is Available

AUDIO PANEL
& CNS

ChartView Database is
Current and Available

AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 8-45 Examples of Power-up Page, ChartView Database

INDEX

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

441

SYSTEM
OVERVIEW

Additional Features

NOTE: A subdued softkey label indicates the function is disabled.

FLIGHT
INSTRUMENTS

The ChartView time critical information can also be found on the AUX - System Status page. The database
CYCLE number, EXPIRES, and DISABLES dates of the ChartView subscription appear in either blue or yellow
text. When the ChartView EXPIRES date is reached, ChartView becomes inoperative 70 days later. This is
shown as the DISABLES date. When the DISABLES date is reached, charts are no longer available for viewing.
The SHW CHRT Softkey label then appears subdued and is disabled until a revised issue of ChartView is
installed.

EIS

Press the DBASE Softkey for scrolling through the database information. Scroll through the database with
the FMS knob or ENT Key.
The ChartView database cycle number shown in the figure, 0822, is deciphered as follows:

AUDIO PANEL
& CNS

08 – Indicates the year 2008
22 – Indicates the 22nd issue of the ChartView database for the year
The EXPIRES date 15–NOV–08 is the date that this database should be replaced with the next issue.

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

The DISABLES date 24–JAN–09 is the date that this database becomes inoperative.

APPENDICES

ADDITIONAL
FEATURES

ChartView
Data

Figure 8-46 AUX – System Status Page, ChartView Current and Available

INDEX

The ChartView database is provided directly from Jeppesen. Refer to Updating Jeppesen Databases in
Appendix B for instructions on revising the ChartView database.

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Additional Features
SYSTEM
OVERVIEW

The other three possible AUX - System Status page conditions are shown here. The EXPIRES date, in yellow,
is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database
cycle is no longer viewable. REGION and CYCLE NOT AVAILABLE in blue, indicate that no ChartView data is
available on the database card or no database card is inserted.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

ChartView Database has Expired, but is not Disabled

ChartView Database is Disabled
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

System is
Configured for
ChartView but
Database is not
Available

APPENDICES

ChartView Database is Not Available

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Figure 8-47 AUX – System Status Page, ChartView Expired, ChartView Disabled, ChartView Not Available

443

SYSTEM
OVERVIEW

Additional Features

8.4 FliteCharts

FLIGHT
INSTRUMENTS

FliteCharts resemble the paper version of National Aeronautical Charting Office (NACO) terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable charts. FliteCharts database
subscription is available from Garmin. Available data includes:
• Arrivals (STAR)
• Approaches
• Departure Procedures (DP)

• Airport Diagrams

EIS

FliteCharts Softkeys

AUDIO PANEL
& CNS

FliteCharts functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest
Airports Page, or Flight Plan Page, pressing the SHW CHRT Softkey displays the available terminal chart and
advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO, DP, STAR, APR, WX, and
GO BACK. The chart selection softkeys appear on the Airport Information Page.
Pressing the GO BACK Softkey reverts to the top level softkeys and previous page.

FLIGHT
MANAGEMENT

Pressing the CHRT OPT Softkey displays the available terminal chart and advances to the next level of
softkeys: ALL, FIT WDTH, FULL SCN, and BACK.
While viewing the CHRT OPT Softkeys, after 45 seconds of softkey inactivity, the system reverts to the chart
selection softkeys.
NOTAMs are not available with FliteCharts. The NOTAM Softkey label appears subdued and is disabled.

HAZARD
AVOIDANCE

SHW CHRT

AFCS

CHRT OPT

CHRT

INFO

STAR

APR

GO BACK

Presssing the GO BACK Softkey returns
to the top-level softkeys and previous page.

ADDITIONAL
FEATURES

ALL

FIT WDTH

FULL SCN

BACK

Pressing the BACK Softkey returns
to the Chart Selection Softkeys.

INDEX

APPENDICES

Figure 8-48 FliteCharts SHW CHRT, Chart Selection, and Chart Option Softkeys

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Additional Features
SYSTEM
OVERVIEW

Terminal Procedures Charts
Selecting Terminal Procedures Charts:

FLIGHT
INSTRUMENTS

While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press the SHW CHRT
Softkey.
Or:

1) Press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart.

EIS

3) Press the ENT Key to display the chart.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

Navigation Map Page OPTIONS Menu

Waypoint Airport Information Page OPTIONS Menu

Figure 8-49 Option Menus

AFCS

When no terminal procedure chart is available, the banner CHART NOT AVAILABLE appears on the screen.
The CHART NOT AVAILABLE banner does not refer to the FliteCharts subscription, but rather the availability
of a particular airport chart selection or procedure for a selected airport.

ADDITIONAL
FEATURES

Figure 8-50 Chart Not Available Banner

APPENDICES

If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner
UNABLE TO DISPLAY CHART is then displayed.

INDEX

Figure 8-51 Unable To Display Chart Banner

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445

SYSTEM
OVERVIEW

Additional Features
When a chart is not available by pressing the SHW CHRT Softkey or selecting a Page Menu Option, charts
may be obtained for other airports from the WPT Pages or Flight Plan Pages.

FLIGHT
INSTRUMENTS

EIS

AUDIO PANEL
& CNS

FLIGHT
MANAGEMENT

4) Turn the small and large FMS Knob to enter the desired airport identifier.
5) Press the ENT Key to complete the airport selection.
6) Turn the large FMS Knob to select the Approach Box.
7) Turn the small FMS Knob to show the approach chart selection choices.

HAZARD
AVOIDANCE

8) Turn either FMS Knob to scroll through the available charts.
9) Press the ENT Key to complete the chart selection.

AFCS

Chart Not
To Scale

ADDITIONAL
FEATURES

Select Desired
Approach Chart
from Menu

APPENDICES

Pan Chart
With the
Joystick

INDEX

Aircraft Not
Shown Icon
Figure 8-52 Approach Information Page, Chart Selection

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Additional Features
SYSTEM
OVERVIEW

While the APPROACH Box is selected using the FMS Knob, the G1000 softkeys are blank. Once the desired
chart is selected, the chart scale can be changed and the chart can be panned using the Joystick. Pressing the
Joystick centers the chart on the screen.

FLIGHT
INSTRUMENTS

The aircraft symbol is not shown on FliteCharts. The Chart Scale Box displays a banner NOT TO SCALE, and
the Aircraft Not Shown Icon is displayed in the lower right corner of the screen.
Pressing the CHRT Softkey alternates between the FliteCharts diagram and the associated map in the WPT
page group. In the example shown, the CHRT Softkey switches between the Charlotte, NC (KCLT) Airport
Diagram and the navigation map on the WPT – Airport Information page.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS

Press CHRT Softkey
to Switch Between
FliteCharts and
Navigation Map Page

ADDITIONAL
FEATURES
APPENDICES

Figure 8-53 CHRT Softkey, Airport Information Page
INDEX

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

447

SYSTEM
OVERVIEW

Additional Features
Pressing the INFO Softkey returns to the airport diagram when the view is on a different chart. If the
displayed chart is the airport diagram, the INFO Softkey has no effect.

EIS

FLIGHT
INSTRUMENTS

Another source for additional airport information is from the INFO Box above the chart or to the right of the
chart (Figure 8-54) for certain airports. This information source is not related to the INFO Softkey. When the
INFO Box is selected using the FMS Knob, the G1000 softkeys are blank. The Charlotte, NC airport has three
additional charts offering information; the Airport Diagram, Alternate Minimums, and Take-off Minimums.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Info Box
Selected

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 8-54 Airport Information Page, INFO View with Airport Information

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

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Additional Features
SYSTEM
OVERVIEW

In the example shown in Figure 8-54, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the
Take-off Minimums and Departure Procedures Chart (Figure 8-55).

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-55 Airport Information Page, TAKE OFF MINIMUMS Selected from INFO View

HAZARD
AVOIDANCE

Pressing the DP Softkey displays the Departure Procedure Chart if available.

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

Figure 8-56 Departure Information Page

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

449

SYSTEM
OVERVIEW

Additional Features

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available.

Figure 8-57 Arrival Information Page

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Pressing the APR Softkey displays the approach chart for the airport if available.

INDEX

Figure 8-58 Approach Information Page

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Additional Features
SYSTEM
OVERVIEW

Pressing the WX Softkey shows the airport weather frequency information, when available, and includes
weather data such as METAR and TAF from the XM Data Link Receiver. Weather information is available only
when an XM Data Link Receiver is installed and the XM Weather subscription is current.

FLIGHT
INSTRUMENTS

Selecting Additional Information:
1) While viewing the Airport Taxi Diagram, press the WX Softkey to display the information windows (AIRPORT,
INFO).
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the INFO Box.

EIS

4) Turn the small FMS Knob to select the INFO Box choices. When the INFO Box is selected the G1000 softkeys
are blank. If multiple choices are available, scroll to the desired choice with the large FMS Knob and press the
ENT Key to complete the selection.

AUDIO PANEL
& CNS

5) Press the FMS Knob again to deactivate the cursor.

FLIGHT
MANAGEMENT

Info Available
on This Airport

HAZARD
AVOIDANCE

WX Info
When
Available

AFCS

Chart Not
To Scale

Figure 8-59 Weather Information Page, WX Softkey Selected

ADDITIONAL
FEATURES

Softkeys are
Blank during
Info Box
Selection

WX Softkey
Selected

APPENDICES

Pressing the GO BACK Softkey reverts to the previous page (Navigation Map Page or Flight Plan Page).

INDEX

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

451

SYSTEM
OVERVIEW

Additional Features

Chart Options
Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-48).

EIS

FLIGHT
INSTRUMENTS

Pressing the ALL Softkey shows the complete chart on the screen.

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Complete
Chart
Shown

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Figure 8-60 Airport Information Page, ALL View Selected

452

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Additional Features
SYSTEM
OVERVIEW

Pressing the FIT WIDTH Softkey fits the width of the chart in the display viewing area. In the example
shown, the chart at close range is replaced with the full width chart.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Press FIT WDTH
Softkey to Show
Full Chart Width
Figure 8-61 Approach Information Page, FIT WDTH Softkey Selected

APPENDICES
INDEX

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

453

SYSTEM
OVERVIEW

Additional Features

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right.

AFCS

HAZARD
AVOIDANCE

Press FULL SCN
Softkey to Switch
Between Chart on
Full Screen and Chart
with Info Window

ADDITIONAL
FEATURES

Figure 8-62 Airport Information Page, Full Screen and Info Window

INDEX

APPENDICES

Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys.

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Additional Features
SYSTEM
OVERVIEW

The full screen view can also be selected by using the page menu option.
Selecting full screen On or Off:

FLIGHT
INSTRUMENTS

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Chart Setup Option

Full Screen On/Off Selection

HAZARD
AVOIDANCE

Figure 8-63 Page Menus

AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

455

SYSTEM
OVERVIEW

Additional Features

Day/Night View

FLIGHT
INSTRUMENTS

FliteCharts can be displayed on a white or black background for day or night viewing. The Day View offers
a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark
environment. When the CHART SETUP Box is selected the G1000 softkeys are blank.
Selecting Day, Night, or Automatic View:
1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.

HAZARD
AVOIDANCE

Figure 8-64 Waypoint Information Page, OPTIONS Menu

3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑65).
4) Turn the small FMS Knob to choose between Day, Auto, and Night Options.

AFCS

ADDITIONAL
FEATURES

The display must be changed in order for the new setting to become active. This may be accomplished by
selecting another page or changing the display range.

INDEX

APPENDICES

6) Press the FMS Knob when finished to remove the Chart Setup Menu.

456

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Additional Features
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-65 Approach Information Page, Day View

HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 8-66 Approach Information Page, Night View

INDEX

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

457

SYSTEM
OVERVIEW

Additional Features

FliteCharts Cycle Number and Expiration Date

FLIGHT
INSTRUMENTS

FliteCharts data is revised every 28 days. Charts are still viewable during a period that extends from the
cycle expiration date to the disabled date. FliteCharts is disabled 180 days after the expiration date and are
no longer available for viewing upon reaching the disabled date. When turning on the G1000, the Power-up
Page indicates any of five different possible criteria for chart availability. These indications are whether the
databases are not configured, not available, current, out of date, or disabled. See the table below for the various
FliteCharts Power-up Page displays and the definition of each.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Power-up Page Display

Definition
Blank Line. G1000 system is not configured for FliteCharts. Contact
a Garmin-authorized service center for configuration.
System is configured for FliteCharts but no chart database is
installed. Refer to Updating Garmin Databases in Appendix B for the
FliteCharts database
Normal operation. FliteCharts database is valid and within current
cycle.

HAZARD
AVOIDANCE

FliteCharts database is beyond the expiration date, but still within
the 180 day viewing period.
FliteCharts database has timed out. Database is beyond 180 days
after expiration date. FliteCharts database is no longer available for
viewing.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

Table 8-2 FliteCharts Power-up Page Annunciations and Definitions

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Additional Features
SYSTEM
OVERVIEW

Examples of four possible Power-up Page messages are shown here. ‘FliteCharts Expires’ plus a date in white,
indicates the chart database is current. ‘Chart data is out of date!’ in yellow, indicates charts are still viewable,
but approaching the disable date.

FLIGHT
INSTRUMENTS

When the 180 day grace period has expired, ‘Chart data is disabled.’ in yellow indicates that the FliteCharts
database has expired and is no longer viewable. ‘Chart Data: N/A’ appears in white if no FliteCharts data is
available on the database card or no database card is inserted.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

FliteCharts Database is Disabled

FliteCharts Database is Not Available

AFCS

FliteCharts Database is
Expired but Still Available

HAZARD
AVOIDANCE

FliteCharts Database is Current
and Available

ADDITIONAL
FEATURES
APPENDICES
INDEX

Figure 8-67 FliteCharts Power-up Page Messages

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

459

SYSTEM
OVERVIEW

Additional Features

NOTE: A subdued softkey label indicates the function is disabled.

FLIGHT
INSTRUMENTS

FliteCharts time critical information can also be found on the AUX - System Status page. The FliteCharts
database REGION, CYCLE number, EFFECTIVE, EXPIRES, and DISABLES dates of the subscription appear in
either blue or yellow text. Dates shown in blue are current data. Dates shown in yellow indicate the data is not
within the current subscription period.

EIS

FliteCharts becomes inoperative 180 days after the FliteCharts EXPIRES date is reached, and is no longer
available for viewing. This date is shown as the DISABLES date. After the disable date the SHW CHRT Softkey
label appears subdued and is unavailable until a revised issue of FliteCharts is installed.
Press the DBASE Softkey for scrolling through the database information. Scroll through the database with
the FMS knob or ENT Key.

AUDIO PANEL
& CNS

The FliteCharts database cycle number shown in the figure, 0807, is deciphered as follows:
08 – Indicates the year 2007
07 – Indicates the seventh issue of the FliteCharts database for the year

FLIGHT
MANAGEMENT

The FliteCharts EFFECTIVE date 05–JUL–08 is the first date that this database is current.
The FliteCharts EXPIRES date 02–AUG–08 is the last date that this database is current.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

The DISABLES date 29–JAN–09 is the date that this database becomes inoperative.

APPENDICES

FliteCharts
Data

INDEX

Figure 8-68 AUX – System Status Page, FliteCharts Current and Available

The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for
instructions on revising the FliteCharts database.

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Additional Features
SYSTEM
OVERVIEW

The other three possible AUX - System Status page conditions are shown here. The EXPIRES date, in yellow,
is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle
is no longer viewable. REGION and CYCLE NOT AVAILABLE in blue, indicate that FliteCharts database is not
available on the database card or no database card is inserted.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

FliteCharts Database has Expired, but is not Disabled

FliteCharts Database is Disabled
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

System is
Configured for
FliteCharts but
Database is not
Installed

APPENDICES

FliteCharts Database is Not Available

190-00592-06 Rev A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Figure 8-69 AUX – System Status Page, FliteCharts Expired,
FliteCharts Disabled, FliteCharts Not Available

461

SYSTEM
OVERVIEW

Additional Features

8.5 XM Radio Entertainment (Optional)

FLIGHT
INSTRUMENTS

Note: Refer to the Hazard Avoidance Section for information about XM Weather products.

The optional XM Radio entertainment feature of the GDL 69A Data Link Receiver is available for the pilot’s and
passengers’ enjoyment. The GDL 69A can receive XM Satellite Radio® entertainment services at any altitude
throughout the Continental U.S. Entertainment audio is not available on the GDL 69 Data Link Receiver.

EIS

XM Satellite Radio offers a variety of radio programming over long distances without having to constantly
search for new stations. Based on signals from satellites, coverage far exceeds land-based transmissions.
XM Satellite Radio services are subscription-based. For more information on specific service packages, visit
www.xmradio.com.

AUDIO PANEL
& CNS

Activating XM Satellite Radio Services
The service is activated by providing XM Satellite Radio with either one or two coded IDs, depending on the
equipment. Either the Audio Radio ID or the Data Radio ID, or both, must be provided to XM Satellite Radio
to activate the entertainment subscription.

FLIGHT
MANAGEMENT

It is not required to activate both the entertainment and weather service subscriptions with the GDL 69A.
Either or both services can be activated. XM Satellite Radio uses one or both of the coded IDs to send an
activation signal that, when received by the GDL 69A, allows it to play entertainment programming.
These IDs are located:

HAZARD
AVOIDANCE

• On the label on the back of the Data Link Receiver
• On the XM Information Page on the MFD (Figure 8-70)
• On the XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N
190-00355-04)

AFCS

Contact the installer if the Data Radio ID and the Audio Radio ID cannot be located.
NOTE: The LOCK Softkey on the XM Information Page (Auxiliary Page Group) is used to save GDL 69A

INDEX

APPENDICES

ADDITIONAL
FEATURES

activation data when the XM services are initially set up. It is not used during normal XM Radio operation,
but there should be no adverse effects if inadvertently pressed during flight. Refer to the GDL 69/69A XM
Satellite Radio Activation Instructions (190-00355-04, Rev F or later) for further information.

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Additional Features
SYSTEM
OVERVIEW

Activating the XM Satellite Radio services:

FLIGHT
INSTRUMENTS

1) Contact XM Satellite Radio through the email address listed on their website (www.xmradio.com) or by the
customer service phone number listed on the website. Follow the instructions provided by XM Satellite Radio
services.
2) Select the Auxiliary Page Group.
3) Select the next to last page in the AUX Page Group.
4) Press the INFO Softkey to display the XM Information Page.
5) Verify that the desired services are activated.

EIS

6) Press the LOCK Softkey.
7) Turn the large FMS Knob to highlight YES.

Data
Radio ID

AUDIO PANEL
& CNS

8) To complete activation, press the ENT Key.

FLIGHT
MANAGEMENT

Audio
Radio ID

HAZARD
AVOIDANCE

Weather
Products
Window

AFCS

Figure 8-70 XM Information Page

LOCK Softkey
is Used to Save
Activation
Data During
Initial Setup

APPENDICES

If XM weather services have not been activated, all the weather product boxes are blank on the XM Information
Page and a yellow Activation Required message is displayed in the center of the Weather Data Link Page (Map
Page Group). The Service Class refers to the groupings of weather products available for subscription.

ADDITIONAL
FEATURES

RADIO
and INFO
Softkeys

INDEX

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SYSTEM
OVERVIEW

Using XM Radio

FLIGHT
INSTRUMENTS

Additional Features

The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite
Radio.

The optional GRC 10 Remote Control Unit provides control of the XM Radio functions idependent of the
MFD controls. See the GRC 10 User’s Guide for details.

Selecting the XM Radio Page:
1) Turn the large FMS Knob to select the Auxiliary Page Group.

EIS

2) Turn the small FMS Knob to select the displayed AUX - XM Information Page.

AUDIO PANEL
& CNS

3) Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled.

FLIGHT
MANAGEMENT

Active
Channel

HAZARD
AVOIDANCE

Channel
List

Volume
Field

AFCS

Categories
Field

ADDITIONAL
FEATURES

Figure 8-71 XM Radio Page

Active Channel and Channel List
The Active Channel Box on the XM Radio Page displays the currently selected channel that the XM Radio
is using.

APPENDICES

The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category.
Channels can be stepped through one at a time or may be selected directly by channel number.
Selecting a channel from the channel list:
1) While on the XM Radio Page, press the CHNL Softkey.

INDEX

2) Press the CH + Softkey to go up through the list in the Channel Box, or move down the list with the
CH – Softkey.

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Additional Features
SYSTEM
OVERVIEW

Or:

1) Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels.
2) Press the ENT Key to activate the selected channel.

FLIGHT
INSTRUMENTS

Selecting a channel directly:
1) While on the XM Radio Page, press the CHNL Softkey.
2) Press the DIR CH Softkey. The channel number in the Active Channel Box is highlighted.

EIS

3) Press the numbered softkeys located on the bottom of the display to directly select the desired channel
number.
4) Press the ENT Key to activate the selected channel.

AUDIO PANEL
& CNS

Category
The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of
channels such as jazz, rock, or news can be selected to list the available channels for a type of music or other
contents. One of the optional categories is PRESETS to view channels that have been programmed.

FLIGHT
MANAGEMENT

Selecting a category:
1) Press the CATGRY Softkey on the XM Radio Page.
2) Press the CAT + and CAT - Softkeys to cycle through the categories.
Or:

HAZARD
AVOIDANCE

Turn the small FMS Knob to display the Categories list. Highlight the desired category with the small FMS Knob
and press the ENT Key. Selecting All Categories places all channels in the list.

AFCS
ADDITIONAL
FEATURES
APPENDICES

Figure 8-72 Categories List
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SYSTEM
OVERVIEW

Additional Features
Presets

FLIGHT
INSTRUMENTS

Up to 15 channels from any category can be assigned a preset number. The preset channels are selected by
pressing the PRESETS and MORE Softkeys. Then the preset channel can be selected directly and added to
the channel list for the Presets category.
Setting a preset channel number:
1) On the XM Radio Page, while listening to an Active Channel that is wanted for a preset, press the PRESETS
Softkey to access the first five preset channels (PS1 - PS5).

EIS

2) Press the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five
channels (PS11 – PS15). Pressing the MORE Softkey repeatedly cycles through the preset channels.
3) Press any one of the (PS1 - PS15) softkeys to assign a number to the active channel.

AUDIO PANEL
& CNS

4) Press the SET Softkey on the desired channel number to save the channel as a preset.

FLIGHT
MANAGEMENT

Press PRESETS to
Access the Preset
Channels Softkeys

Press MORE to Cycle
Through the Preset
Channels

HAZARD
AVOIDANCE

Press SET to
Save Each
Preset Channel

Figure 8-73 Accessing and Selecting XM Preset Channels

Pressing the BACK Softkey, or waiting during 45 seconds of softkey inactivity, returns the system to the top
level softkeys.

AFCS

Volume
Radio volume is shown as a percentage of full volume. Volume level is controlled by pressing the VOL
Softkey, which brings up the MUTE Softkey and the volume increase and decrease softkeys.

ADDITIONAL
FEATURES

Adjusting the volume:
1) With the XM Radio Page displayed, press the VOL Softkey.

APPENDICES

2) Press the VOL – Softkey to reduce volume or press the VOL + Softkey to increase volume. (Once the VOL
Softkey is pressed, the volume can also be adjusted using the small FMS Knob.)

INDEX

3) Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to unmute the audio.

Figure 8-74 Volume Control

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Additional Features
SYSTEM
OVERVIEW

8.6 Scheduler

FLIGHT
INSTRUMENTS

The Scheduler feature can be used to enter and display reminder messages (e.g., Change oil, Switch fuel tanks,
or Altimeter-Transponder Check) in the Messages Window on the PFD. Messages can be set to display based on
a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently
whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset
to the original timer value once the message is displayed. When power is cycled, all messages are retained until
deleted, and message timer countdown is resumed.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-75 Scheduler (Utility Page)

HAZARD
AVOIDANCE

Entering a scheduler message:
1) Select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the first empty scheduler message naming field.

AFCS

4) Use the FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT
Key.
5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type.

ADDITIONAL
FEATURES

6) Turn the small FMS Knob to select the message type:
• Event—Message issued at the specified date/time
• One-time—Message issued when the message timer reaches zero (default setting)

APPENDICES

• Periodic—Message issued each time the message timer reaches zero
7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
8) For periodic and one-time message, use the FMS Knob to enter the timer value (HH:MM:SS) from which to
countdown and press the ENT Key.

INDEX

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SYSTEM
OVERVIEW

Additional Features
9) For event-based messages:
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key.

FLIGHT
INSTRUMENTS

b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key.
10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message.

Deleting a scheduler message:
1) Select the AUX - Utility Page.

EIS

2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted.

AUDIO PANEL
& CNS

4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored.
5) Press the ENT Key while the message line is cleared to clear the message text.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Scheduler messages appear in the Messages Window on the PFD. When a scheduler message is waiting, the
ALERTS Softkey label changes to ADVISORY. Pressing the ADVISORY Softkey opens the Messages Window
and acknowledges the scheduler message. The softkey label reverts to ALERTS when pressed. Pressing the
ALERTS Softkey again removes the Messages Window from the display, and the scheduler message is deleted
from the message queue.

INDEX

APPENDICES

Figure 8-76 PFD Messages Window

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Additional Features
SYSTEM
OVERVIEW

8.7 Electronic Checklists

FLIGHT
INSTRUMENTS

NOTE: The checklists presented here are for example only and may not reflect checklists actually available

for the Diamond DA40. This material is not intended to replace the checklist information presented in the
AFM or the Pilot Safety and Warning Supplements document.
NOTE: Garmin is not responsible for the content of checklists. Diamond DA40 checklists are created,

modified, and updated by the aircraft manufacturer.
EIS

The optional checklist functions are displayed on two levels of softkeys that are available on any MFD page.
(Optional)
SYSTEM

MAP

DCLTR

DONE

EXIT

AUDIO PANEL
& CNS

SYSTEM

SHW CHRT CHKLIST

EMERGCY

FLIGHT
MANAGEMENT

The DONE Softkey label changes to UNDO
when the checklist item is already checked.

Figure 8-77 Checklist Softkeys

HAZARD
AVOIDANCE

The MFD is able to display optional electronic checklists which allow a pilot to quickly find the proper
procedure on the ground and during each phase of flight. The G1000 accesses the checklists from an SD
card inserted into the bezel slot. If the SD card contains an invalid checklist file or no checklist, the Power-up
Page messages display Invalid Checklist File or Checklist File Not Present and the CHKLIST Softkey is not
available.
Accessing and navigating checklists:

AFCS

1) From any page on the MFD, press the CHKLIST Softkey.
2) Turn the large FMS Knob to select the GROUP field.

ADDITIONAL
FEATURES

3) Turn the small FMS Knob to select the desired procedure and press the ENT Key.
4) Turn the large FMS Knob to select the Checklist field.
5) Turn the FMS Knob to select the desired checklist and press the ENT Key.

The following colors are used for checklist items:
• Blue - Items has not been highlighted

• Green - Item has been checked

• White - Item is highlighted for checking

• Yellow - Warning notes

APPENDICES

6) Turn the FMS Knob to scroll through the checklist and highlight the desired checklist item. A hollow white box
is used for the checkmark.

190-00592-06 Rev A

INDEX

7) Press the ENT Key or DONE Softkey to check the highlighted checklist item. The line item turns green and a
checkmark is placed in the box next to it. The next line item is automatically highlighted for checking.

Press the CLR Key to remove a check mark from an item.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

469

SYSTEM
OVERVIEW

Additional Features
8) Once the last item in a checklist is checked, the next highlighted item is, Go to the next checklist? Press the ENT
Key to advance to the next checklist displayed.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

9) Press the EXIT Softkey or hold down the CLR Key momentarily to exit the Checklist Page and return to the page
last viewed.

INDEX

APPENDICES

Figure 8-78 Sample Checklist

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Additional Features
SYSTEM
OVERVIEW

Immediately accessing emergency procedures:
1) From any page, press the CHKLIST Softkey.
2) Press the EMERGCY Softkey.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES

Figure 8-79 Emergency Checklist Page Example

APPENDICES
INDEX

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SYSTEM
OVERVIEW

Additional Features

8.8 Flight Data Logging

FLIGHT
INSTRUMENTS

The G1000 has the ability to record certain flight and engine parameters on an SD card with a maximum size of
four-gigabytes. A two-gigabyte SD card containing no other data, is capable of storing 2,000 hours of data. The
following data will automatically be recorded once every second as long as the system is operating and an SD card
resides in the top card slot of the MFD.
• GPS Horizontal Protection level
• GPS vertical alert limit
• GPS Vertical Speed
• Ground Speed
• Ground Track Magnetic
• Horizontal CDI
• HSI Source
• Indicated Air Speed
• Lateral/Y/Right Acceleration
• Local 24hr Time
• Local Date
• Magnetic Heading
• Magnetic Variation
• Manifold Pressure
• NAV1 Frequency
• NAV2 Frequency
• Normal/Z/Up Acceleration
• Oil Pressure
• Oil Temperature
• Outside Air Temperature
• Selected Course
• True Airspeed
• UTC time
• Vertical CDI
• Vertical Speed
• WAAS GPS horizontal protection level
• WAAS GPS vertical protection level
• Wind Direction
• Wind Speed

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

• Active Waypoint
• Attitude Pitch Angle
• Attitude Roll Angle
• Autopilot (AP) Engaged
• Baro Adjustment/Correction
• Baro-Corrected Altitude
• Battery AMP
• Battery Volts
• Bearing to Next Waypoint
• Carburetor Temperature
• COM1 Frequency
• COM2 Frequency
• Current Position
• Cylinder head temperature, cylinders 1 - 4
• Distance to Next Waypoint
• Engine RPM
• Exhaust Gas Temperature, cylinders 1-4
• Fuel Flow
• Fuel Pressure
• Fuel Quanity Left
• Fuel Quanity Right
• GFC 700 Pitch Command
• GFC 700 Pitch Mode
• GFC 700 Roll Command
• GFC 700 Roll Mode
• GPS Altitude
• GPS Altitude Relative to Mean Sea Level
• GPS Fix
• GPS Horizontal Alert Limit

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Additional Features
SYSTEM
OVERVIEW

The file containing the recorded data will appear in the format shown in Figure 8-80. This file can be imported
into most computer spreadsheet applications.

Local 24hr Time
HHMMSS

FLIGHT
INSTRUMENTS

Local Date
YYMMDD

Nearest Airport
(A blank will be
inserted if no
airport is found)

log_090210_104506_KIXD.csv
EIS

Figure 8-80 Log File Format
AUDIO PANEL
& CNS

Data logging status can be monitored on the AUX-UTILITY Page.

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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SYSTEM
OVERVIEW

Additional Features

8.9 Abnormal Operation

FLIGHT
INSTRUMENTS

SVS Troubleshooting
SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is
disabled when valid attitude or heading data is not available for the display. In case of invalid SVS data, the PFD
display reverts to the standard blue-over-brown attitude display.
SVS becomes disabled without the following data resources:

EIS

• Attitude data
• Heading data
• GPS position data
AUDIO PANEL
& CNS

• 9 Arc-second Terrain data
• Obstacle data
• TAWS function is not available, in test mode, or failed

FLIGHT
MANAGEMENT

• The position of the aircraft exceeds the range of the terrain database.

Reversionary Mode

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

SVS can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching
to Reversionary Mode, SVS will take up to 30 seconds to be displayed. The standard, non-SVS PFD display will
be shown in the interim.

Figure 8-81 SVS Reversionary Mode

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Additional Features
SYSTEM
OVERVIEW

Unusual Attitudes

FLIGHT
INSTRUMENTS

Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to fly to
correct the unusual attitude condition. The display shows either a brown or blue colored bar at the top or
bottom of the screen to represent earth or sky. This is intended to prevent losing sight of the horizon during
extreme pitch attitudes.

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure 8-82 Unusual Attitude Display

The blue colored bar is also displayed when terrain gradient is great enough to completely fill the display.

HAZARD
AVOIDANCE

Blue Band

AFCS

Terrain
Completely
Fills Display

ADDITIONAL
FEATURES

Figure 8-83 Blue Sky Bar with Full Display Terrain

APPENDICES
INDEX

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475

SYSTEM
OVERVIEW

Additional Features

GDL 69/69A Data Link Receiver Troubleshooting
Some quick troubleshooting steps listed below can be performed to find the possible cause of a failure.

FLIGHT
INSTRUMENTS

• Ensure the owner/operator of the aircraft in which the Data Link Receiver is installed has subscribed to XM
• Ensure the XM subscription has been activated
• Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver
• Ensure that nothing is plugged into the Aux Audio In jack because this would prevent XM radio from being
heard

EIS

For troubleshooting purposes, check the LRU Information Box on the AUX - System Status Page for Data Link
Receiver (GDL 69/69A) status, serial number, and software version number. If a failure has been detected in the
GDL 69/69A the status is marked with a red X.

AUDIO PANEL
& CNS

Selecting the System Status Page:
1) Turn the large FMS Knob to select the AUX Page Group.

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

2) Turn the small FMS Knob to select the System Status Page (the last page in the AUX Page Group).

INDEX

Figure 8-84 LRU Information Window on System Status Page

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Additional Features
SYSTEM
OVERVIEW

If a failure still exists, the following messages may provide insight as to the possible problem:

NO SIGNAL
LOADING
OFF AIR
---

Message Location
XM Radio Page - active channel field
XM Radio Page - active channel field
XM Radio Page - active channel field
Weather Datalink Page - center of page
XM Radio Page - active channel field
XM Radio Page - active channel field
XM Radio Page - active channel field

Description
Data Link Receiver antenna error; service required
Data Link Receiver updating encryption code

FLIGHT
INSTRUMENTS

Message
CHECK ANTENNA
UPDATING

Loss of signal; signal strength too low for receiver

EIS

Acquiring channel audio or information
Channel not in service
Missing channel information
No communication from Data Link Receiver
WEATHER DATA LINK FAILURE Weather Datalink Page - center of page
within last 5 minutes
ACTIVATION REQUIRED
Weather Datalink Page - center of page XM subscription is not activated

AUDIO PANEL
& CNS

Table 8-3 GDL 69/69A Data Link Receiver Error Messages

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

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477

INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Additional Features

Blank Page

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Appendix A

SYSTEM
OVERVIEW

Annunciations and Alerts
Note: The Aircraft Flight Manual (AFM) supersedes information found in this document.

FLIGHT
INSTRUMENTS

The G1000 Alerting System conveys alerts using the following:

EIS

• Annunciation Window: The Annunciation Window displays abbreviated annunciation text. Text color is
based on alert levels described in the following section. The Annunciation Window is located to the right
of the Altimeter and Vertical Speed Indicator. All aircraft annunciations can be displayed simultaneously
in the Annunciation Window. A white horizontal line separates annunciations that are acknowledged from
annunciations that are not yet acknowledged. Higher priority annunciations are displayed towards the top of
the window.

AUDIO PANEL
& CNS

• Alerts Window: The Alerts Window displays text messages for up to 64 prioritized alert messages. Pressing
the ALERTS Softkey displays the Alerts Window. Pressing the ALERTS Softkey a second time removes the
Alerts Window from the display. When the Alerts Window is displayed, the FMS Knob can be used to scroll
through the alert message list.

FLIGHT
MANAGEMENT

• Softkey Annunciation: During certain alerts, the ALERTS Softkey may appear as a flashing annunciation
to accompany an alert. The ALERTS Softkey assumes a new label consistent with the alert level (WARNING,
CAUTION, or ADVISORY). By selecting the softkey when flashing an annunciation, the alert is acknowledged.
The softkey label then returns to ALERTS. If alerts are still present, the ALERTS label is displayed in white
with black text. Selecting the ALERTS Softkey a second time views the alert text messages.
• System Annunciations: Typically, a large red ‘X’ appears over instruments whose information is supplied by
a failed Line Replaceable Unit (LRU). See the G1000 System Annunciations Section for more information.

HAZARD
AVOIDANCE

System
Annunciation
(Red ‘X’)

AFCS
ADDITIONAL
FEATURES

Annunciation
Window

Alerts
Window

APPENDICES

Softkey
Annunciation

INDEX

Figure A-1 G1000 Alerting System

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SYSTEM
OVERVIEW

Appendix A
• Audio Alerting System: The G1000 System issues audio alert tones when specific system conditions are met.
See the Alert Level Definitions Section for more information. The annunciation tone may be tested from the
AUX - System Status Page.

FLIGHT
INSTRUMENTS

Testing the system annunciation tone:
1) Use the FMS Knob to select the AUX - System Status Page.
2) Select the ANN TEST Softkey.

Or:

EIS

a) Press the MENU Key.

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key.

Press to Test Annunciation Tone

ADDITIONAL
FEATURES

Figure A-2 Annunciation Tone Testing
(AUX-System Status Page)

Alert Level Definitions
The G1000 Alerting System, as installed in Diamond DA40/40F aircraft, uses three alert levels.

APPENDICES

• WARNING: This level of alert requires immediate attention.
Warning alert text is shown in red in the Annunciation Window and is accompanied by a continuous chime
and a flashing ‘WARNING’ Softkey annunciation. Pressing the WARNING Softkey acknowledges the presence
of the warning alert and stops the aural chime.

INDEX

• CAUTION: This level of alert indicates the existence of abnormal conditions on the aircraft that may require
intervention.

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Appendix A
SYSTEM
OVERVIEW

Caution alert text is shown in yellow in the Annunciation Window and is accompanied by a single chime
and a flashing ‘CAUTION’ Softkey annunciation. Pressing the CAUTION Softkey acknowledges the presence
of the caution alert.

FLIGHT
INSTRUMENTS

• ANNUNCIATION OR MESSAGE ADVISORY: This level of alert provides general information.
Annunciation alert text is shown in white in the Annunciation Window; no aural tone is generated. An
annunciation alert is accompanied by a flashing ADVISORY Softkey annunciation. Pressing the ADVISORY
Softkey acknowledges the presence of the annunciation alert.

EIS

Message advisory alerts do not issue annunciations in the Annunciation Window. Instead, message advisory
alerts only issue a flashing ‘ADVISORY’ Softkey annunciation. Selecting the ADVISORY Softkey acknowledges
the presence of the message advisory alert and displays the alert text message in the Alerts Window.

AUDIO PANEL
& CNS

Figure A-3 Softkey Annunciation (ALERTS Softkey Labels)

Aircraft Alerts

Audio Alert

Continuous Aural Tone

AFCS

None

ADDITIONAL
FEATURES

Single Aural Tone

APPENDICES

None

Alerts Window Message
Oil pressure is below 25 psi.
Fuel pressure is below 14 psi. (1.0 psi on DA40F)
Fuel pressure is greater than 35 psi. (8 psi on DA40F)
Alternator failed. Battery is only elec source.
Starter is engaged.
Canopy and/or rear door is not closed and locked.
Autopilot automatic trim has failed.
Left fuel quantity is less than 3 gallons.
Right fuel quantity is less than 3 gallons
On-board voltage is below 24 V.
Pitot heat is inoperative.
Pitot heat is off.
PFD FAN FAIL – The cooling fan for the PFD is inoperative.
MFD FAN FAIL – The cooling fan for the MFD is inoperative.
GIA FAN FAIL – The cooling fan for the GIAs is inoperative.

HAZARD
AVOIDANCE

Annunciation Window Text
OIL PRES LO
FUEL PRES LO*
FUEL PRES HI*
ALTERNATOR
STARTER ENGD
DOOR OPEN
TRIM FAIL**
L FUEL LOW
R FUEL LOW
LOW VOLTS
PITOT FAIL
PITOT OFF

FLIGHT
MANAGEMENT

The following alerts are configured specifically for the Diamond DA40/40F. Red annunciation window text
signifies warnings and yellow, cautions. See the Aircraft Flight Manual Supplement (AFMS) for recommended
pilot actions.

None

* Values differ for the DA40F; refer to the Aircraft Flight Manual Supplement (AFMS) for more information.
** KAP 140 installations only.

INDEX

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SYSTEM
OVERVIEW

Appendix A

Voice Alerts

FLIGHT
INSTRUMENTS

The following audio alerts are announced by the system using a voice of male or female gender. If the
optional Terrain Awareness and Warning System is installed, voice alerts are also generated (refer to the TAWS
Alerts section).

AUDIO PANEL
& CNS

EIS

Voice Alert
“Minimums, Minimums”
“Vertical Track”
“Traffic”
“Traffic Not Available”
“Traffic, Traffic”
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”

Alert Trigger
Issued when the aircraft transitions through the minimum descent altitude/decision height (MDA/DH)
Aircraft is one minute from Top of Descent - issued only when vertical navigation is enabled
TIS voice alert - issued when a Traffic Advisory (TA) is issued
TIS voice alert - issued when the TIStraffic system fails or cannot communicate
TAS voice alert - issued when a Traffic Advisory (TA) is issued
TAS voice alert - issued when the TAS passes a pilot-initiated self test
TAS voice alert - issued when the TAS fails a pilot-initiated self test

FLIGHT
MANAGEMENT

Selecting the audio alert voice:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the voice in the Audio Alert Box.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

4) Turn the small FMS Knob to select the desired voice, press the ENT Key.

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Appendix A
SYSTEM
OVERVIEW

G1000 System Annunciations
NOTE: Upon power-up, certain windows remain invalid as G1000 equipment begins to initialize. All windows

FLIGHT
INSTRUMENTS

should be operational within one minute of power-up. If any window continues to remain flagged, the
G1000 System should be serviced by a Garmin-authorized repair facility.
When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with
the failed data (refer to Figure B-1 for all possible flags and the responsible LRUs). Refer to the Aircraft Flight
Manual (AFM) for additional information regarding pilot responses to these annunciations.

EIS

GIA 63/63W Integrated Avionics Units

AUDIO PANEL
& CNS

GDC 74A
Air Data
Computer

FLIGHT
MANAGEMENT

Database
Mismatch in
PFD and MFD

GEA 71
Engine
Airframe Unit
OR
GIA 63/63W
Integrated
Avionics Unit

GRS 77 AHRS
OR
GMU 44
Magnetometer

GDC 74A
Air Data
Computer

HAZARD
AVOIDANCE

GIA 63/63W
Integrated
Avionics Units

GTX 33 Transponder OR
GIA 63/63W Integrated Avionics Units
AFCS

Figure A-4 G1000 System Failure Annunciations

ADDITIONAL
FEATURES

The status of detected LRUs can be checked on the AUX - System Status Page (Figure A-2). Active LRUs
are indicated by green check marks; failed, by red ‘X’s. Failed LRUs should be noted and a service center or
Garmin-authorized dealer informed.
Viewing LRU information:

APPENDICES

1) Use the FMS Knob to select the AUX - System Status Page.
2) To place the cursor in the ‘LRU Info’ Box,
a) Select the LRU Softkey.
Or:

INDEX

a) Press the MENU Key.
b) With ‘Select LRU Window’ highlighted, press the ENT Key.
3) Use the FMS Knob to scroll through the box to view LRU status information.

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483

SYSTEM
OVERVIEW

Appendix A
System Annunciation

Comment

System Annunciation

FLIGHT
INSTRUMENTS

Attitude and Heading
Reference System is aligning.

Display system is not receiving
vertical speed input from the
air data computer.

AUDIO PANEL
& CNS

EIS

Display system is not receiving
attitude information from the
AHRS.

Display system is not receiving
valid heading input from AHRS.
Display system is not receiving
altitude input from the air data
computer.

FLIGHT
MANAGEMENT

AHRS calibration incomplete or
configuration module failure.

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

This annunciation is seen only
when the autopilot is engaged.
The annunciation indicates an
AHRS monitor has detected
an abnormal flight parameter,
possibly caused by strong
turbulence. In this case, the
situation should correct itself
within a few seconds. If there
is an actual failure, a red “X”
soon appears over the Attitude
Indicator.
GPS information is either
not present or is invalid for
navigation use. Note that
AHRS utilizes GPS inputs
during normal operation.
AHRS operation may be
degraded if GPS signals are not
present (see AFM).

Comment

Other Various Red X
Indications

Display system is not receiving
valid true airspeed information
from air data computer.
Display system is not receiving
valid OAT information from air
data computer.
Display system is not receiving
valid transponder information.
Different versions of GDU
software are installed in the
PFD and MFD. This can also
indicate different versions of the
navigation database installed
in the PFD and MFD. In some
circumstances, a cross-talk error
between the PFD and MFD can
cause this annunciation.
A red ‘X’ through any other
display field (such as engine
instrumentation fields)
indicates that the field is not
receiving valid data.

INDEX

Display system is not receiving
airspeed input from air data
computer.

484

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix A
SYSTEM
OVERVIEW

G1000 System Message Advisories
NOTE: This section provides information regarding G1000 message advisories that may be displayed by the

FLIGHT
INSTRUMENTS

system. Knowledge of the aircraft, systems, flight conditions, and other existing operational priorities must
be considered when responding to a message.
This section describes various G1000 System message advisories. Certain messages are issued due to an LRU
or LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as
shown previously in the G1000 System Annunciations section.

The PFD and/or MFD self-test has detected a problem. The G1000 system should be
serviced.

FLIGHT
MANAGEMENT

The PFD and/or MFD has incorrect software installed. The G1000 system should be
serviced.

HAZARD
AVOIDANCE

The PFD configuration settings do not match backup configuration memory. The
G1000 system should be serviced.
The MFD configuration settings do not match backup configuration memory. The
G1000 system should be serviced.
The MFD and PFD have different software versions installed. The G1000 system
should be serviced.

AFCS

The PFD and/or MFD is overheating and is reducing power consumption by dimming
the display. If problem persists, the G1000 system should be serviced.

ADDITIONAL
FEATURES

A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing
it several times. The G1000 system should be serviced if the problem persists.

APPENDICES

The PFD1 configuration module backup memory has failed. The G1000 system should
be serviced.
The PFD1 voltage is low. The G1000 system should be serviced.

INDEX

190-00592-06 Rev. A

Comments
The pilot profile data was lost. System reverts to default pilot profile and settings. The
pilot may reconfigure the MFD & PFD with preferred settings, if desired.
The MFD and PFD are not communicating with each other. The G1000 system should
be serviced.

AUDIO PANEL
& CNS

Message Advisory
DATA LOST – Pilot stored data was
lost. Recheck settings.
XTALK ERROR – A flight display
crosstalk error has occurred.
PFD1 SERVICE – PFD1 needs service.
Return unit for repair.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MANIFEST – PFD1 software
mismatch, communication halted.
MANIFEST – MFD1 software
mismatch, communication halted.
PFD1 CONFIG – PFD1 config error.
Config service req’d.
MFD1 CONFIG – MFD1 config error.
Config service req’d.
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [key name] is
stuck.
MFD1 KEYSTK – MFD1 [key name]
is stuck.
CNFG MODULE – PFD1 configuration
module is inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage

EIS

Primary Flight Display & Multi Function Display

The MFD voltage is low. The G1000 system should be serviced.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

485

Appendix A
SYSTEM
OVERVIEW

Databases

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Message Advisory
MFD1 DB ERR – MFD1 aviation
database error exists.
PFD1 DB ERR – PFD1 aviation
database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
MFD1 DB ERR – MFD1 airport terrain
database error exists.
PFD1 DB ERR – PFD1 airport terrain
database error exists.
MFD1 DB ERR – MFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 airport
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
MFD1 DB ERR – MFD1 FliteCharts
database error exists.

486

Comments
The MFD and/or PFD detected a failure in the aviation database. Attempt to reload
the aviation database. If problem persists, the G1000 system should be serviced.

The MFD and/or PFD detected a failure in the basemap database.

The MFD and/or PFD detected a failure in the terrain database. Ensure that the
terrain card is properly inserted in display. Replace terrain card. If problem persists,
The G1000 system should be serviced.

The terrain database is present on another LRU, but is missing on the specified LRU.

The MFD and/or PFD detected a failure in the obstacle database. Ensure that the data
card is properly inserted. Replace data card. If problem persists, The G1000 system
should be serviced.

The obstacle database is present on another LRU, but is missing on the specified LRU.

The MFD and/or PFD detected a failure in the airport terrain database. Ensure that
the data card is properly inserted. Replace data card. If problem persists, The G1000
system should be serviced.
The airport terrain database is present on another LRU, but is missing on the specified
LRU.
The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the
data card is properly inserted. Replace data card. If problem persists, The G1000
system should be serviced.
The MFD and/or PFD detected a failure in the ChartView database (optional feature).
Ensure that the data card is properly inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
The MFD and/or PFD detected a failure in the FliteCharts database (optional feature).
Ensure that the data card is properly inserted. Replace data card. If problem persists,
The G1000 system should be serviced.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix A

Comments
The PFD and MFD have different aviation database versions installed. Crossfill is off.
Install correct aviation database version in both displays.
The PFD and MFD have different aviation database types installed (Americas,
European, etc.). Crossfill is off. Install correct aviation database type in both displays.
The PFD and MFD have different terrain database versions installed. Install correct
terrain database version in both displays.
The PFD and MFD have different terrain database types installed. Install correct
terrain database type in both displays.
The PFD and MFD have different obstacle database versions installed. Install correct
obstacle database version in both displays.
The PFD and MFD have different airport terrain databases installed. Install correct
airport terrain database in both displays.

FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS

Message Advisory
DB MISMATCH – Aviation database
version mismatch. Xtalk is off.
DB MISMATCH – Aviation database
type mismatch. Xtalk is off.
DB MISMATCH – Terrain database
version mismatch.
DB MISMATCH – Terrain database
type mismatch.
DB MISMATCH – Obstacle database
version mismatch.
DB MISMATCH – Airport Terrain
database mismatch.

SYSTEM
OVERVIEW

Databases (cont.)

GMA 1347 Audio Panel

The audio panel has incorrect software installed. The G1000 system should be serviced.

HAZARD
AVOIDANCE

GMA1 CONFIG – GMA1 config error.
Config service req’d.
MANIFEST – GMA1 software
mismatch, communication halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.

Comments
The audio panel self-test has detected a failure. The audio panel is unavailable. The
G1000 system should be serviced.
The audio panel configuration settings do not match backup configuration memory.
The G1000 system should be serviced.

FLIGHT
MANAGEMENT

Message Advisory
GMA1 FAIL – GMA1 is inoperative.

The audio panel self-test has detected a problem in the unit. Certain audio functions may
still be available, and the audio panel may still be usable. The G1000 system should be
serviced when possible.

Comments
The GEA1 configuration settings do not match those of backup configuration memory.
The G1000 system should be serviced.
The #1 GEA 71 has incorrect software installed. The G1000 system should be
serviced.

ADDITIONAL
FEATURES

Message Advisory
GEA1 CONFIG – GEA1 config error.
Config service req’d.
MANIFEST – GEA1 software
mismatch, communication halted.

AFCS

GEA 71 Engine/Airframe Unit

GDC 74A Air Data Computer
The GDC 74A has incorrect software installed. The G1000 system should be serviced.
GDC1 is reporting that the altitude error correction is unavailable.

INDEX

190-00592-06 Rev. A

Comments

APPENDICES

Message Advisory
MANIFEST – GDC1 software
mismatch, communication halted.
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.

GDC1 is reporting that the airspeed error correction is unavailable.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

487

SYSTEM
OVERVIEW

Appendix A
GIA 63 Integrated Avionics Unit

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.

488

Comments
The GIA1 and/or GIA2 configuration settings do not match backup configuration
memory. The G1000 system should be serviced.

The GIA1 and/or GIA2 have an error in the audio configuration. The G1000 system
should be serviced.

The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to
warm up to operating temperature.

The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000 system
should be serviced.

The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system
should be serviced.

The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should be
serviced.
The system has detected an over temperature condition in COM1 and/or COM2. The
transmitter will operate at reduced power. If the problem persists, the G1000 system
should be serviced.
The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may
still be usable. The G1000 system should be serviced when possible.
The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or
“pressed”) position. Press the PTT switch again to cycle its operation.
If the problem persists, the G1000 system should be serviced.
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”)
position. Press the transfer switch again to cycle its operation. If the problem
persists, the G1000 system should be serviced.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix A
SYSTEM
OVERVIEW

GIA 63 (Cont.)

Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Displayed after passing the first waypoint of a true north approach when the nav
angle is set to ‘AUTO’.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is
unavailable. The G1000 system should be serviced.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be serviced.

HAZARD
AVOIDANCE

A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be serviced.

AFCS

The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”)
state. Press the transfer switch again to cycle its operation. If the problem persists,
the G1000 system should be serviced.

ADDITIONAL
FEATURES

A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000
system should be serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver
may still be available. The G1000 system should be serviced when possible.

APPENDICES

G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.

Loss of GPS navigation due to position error.

FLIGHT
MANAGEMENT

G/S2 FAIL – G/S2 is inoperative.

Loss of GPS navigation due to insufficient satellites.

AUDIO PANEL
& CNS

GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
GPS2 SERVICE – GPS2 needs service.
Return unit for repair.
NAV1 SERVICE – NAV1 needs service.
Return unit for repair.
NAV2 SERVICE – NAV2 needs service.
Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 FAIL – G/S1 is inoperative.

Loss of GPS integrity monitoring.

EIS

GPS2 FAIL – GPS2 is inoperative.

Comments
GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity
Monitoring (RAIM) from the FAF to the MAP waypoints.

FLIGHT
INSTRUMENTS

Message
RAIM UNAVAIL – RAIM is not
available from FAF to MAP waypoints.
LOI – GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach.
TRUE APR – True north approach.
Change HDG reference to TRUE.
GPS1 FAIL – GPS1 is inoperative.

INDEX

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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

489

Appendix A
SYSTEM
OVERVIEW

GIA 63W Integrated Avionics Unit

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Message Advisory
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.

490

Comments
The GIA1 and/or GIA2 configuration settings do not match backup configuration
memory. The G1000 system should be serviced.

The GIA1 and/or GIA2 have an error in the audio configuration. The G1000 system
should be serviced.

The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to
warm up to operating temperature.

The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000 system
should be serviced.

The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system
should be serviced.

A GIA mismatch has been detected, where only one is WAAS capable.

The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should be
serviced.
The system has detected an over temperature condition in COM1 and/or COM2. The
transmitter operates at reduced power. If the problem persists, the G1000 system
should be serviced.
The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may
still be usable. The G1000 system should be serviced when possible.
The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or
“pressed”) position. Press the PTT switch again to cycle its operation.
If the problem persists, the G1000 system should be serviced.

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix A
SYSTEM
OVERVIEW

GIA 63W (Cont.)
Comments
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”)
position. Press the transfer switch again to cycle its operation. If the problem
persists, the G1000 system should be serviced.

FLIGHT
INSTRUMENTS

GPS integrity is insufficient for the current phase of flight.
Loss of GPS navigation due to insufficient satellites.

EIS

Loss of GPS navigation due to position error.
AUDIO PANEL
& CNS

Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Use LNAV minima when approach is downgraded.

FLIGHT
MANAGEMENT

Displayed after passing the first waypoint of a true north approach when the nav
angle is set to ‘MAGNETIC’.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be serviced.

HAZARD
AVOIDANCE

A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be serviced.
AFCS

ADDITIONAL
FEATURES

A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000
system should be serviced.

APPENDICES

Message Advisory
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
LOI – GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach.
APR DWNGRADE – Approach
downgraded.
TRUE APR – True north approach.
Change HDG reference to TRUE.
GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
GPS2 SERVICE – GPS2 needs service.
Return unit for repair.
NAV1 SERVICE – NAV1 needs service.
Return unit for repair.
NAV2 SERVICE – NAV2 needs service.
Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 FAIL – G/S1 is inoperative.
G/S2 FAIL – G/S2 is inoperative.
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.

A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver
may still be available. The G1000 system should be serviced when possible.

INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

491

SYSTEM
OVERVIEW

Appendix A
GTX 33 Transponder

EIS

FLIGHT
INSTRUMENTS

Message Advisory
XPDR1 CONFIG – XPDR1 config error.
Config service req’d.
MANIFEST – GTX1 software
mismatch, communication halted.
XPDR1 SRVC – XPDR1 needs service.
Return unit for repair.
XPDR1 FAIL – XPDR1 is inoperative.

Comments
The transponder configuration settings do not match those of backup configuration
memory. The G1000 system should be serviced.
The transponder has incorrect software installed. The G1000 system should be
serviced.
The #1 transponder should be serviced when possible.
There is no communication with the #1 transponder.

GRS 77 Attitude and Heading Reference System
Comments
The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS
relies on GPS information to augment the lack of airspeed. The G1000 system should
be serviced.
AHRS1 GPS – AHRS1 using backup
The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000
GPS source.
system should be serviced when possible.
AHRS1 GPS – AHRS1 not receiving
The #1 AHRS is not receiving any or any useful GPS information. Check AFMS
any GPS information.
limitations. The G1000 system should be serviced.
AHRS1 GPS – AHRS1 not receiving
The #1 AHRS is not receiving backup GPS information. The G1000 system should be
backup GPS information.
serviced.
AHRS1 GPS – AHRS1 operating
The #1 AHRS is operating exclusively in no-GPS mode. The G1000 system should be
exclusively in no-GPS mode.
serviced.
AHRS MAG DB – AHRS magnetic
The #1 AHRS earth magnetic field model is out of date. Update magnetic field model
model database version mismatch.
when practical.
AHRS1 SRVC – AHRS1 Magnetic-field The #1 AHRS earth magnetic field model is out of date. Update magnetic field model
model needs update.
when practical.
GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for approved AHRS operation. Heading is
South, no magnetic compass.
flagged as invalid.
MANIFEST – GRS1 software
The #1 AHRS has incorrect software installed. The G1000 system should be serviced.
mismatch, communication halted.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Message Advisory
AHRS1 TAS – AHRS1 not receiving
valid airspeed.

GDL 69/69A Satellite Datalink Receiver

APPENDICES

Message Advisory
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GDL69 FAIL – GDL 69 has failed.

Comments
GDL 69 configuration settings do not match those of backup configuration memory.
The G1000 system should be serviced.
A failure has been detected in the GDL 69. The receiver is unavailable. The G1000
system should be serviced.

INDEX

MANIFEST – GDL software mismatch,
The GDL 69 has incorrect software installed. The G1000 system should be serviced.
communication halted.

492

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix A

Comments
A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000 system should be serviced.

FLIGHT
INSTRUMENTS

Message Advisory
HDG FAULT – AHRS1 magnetometer
fault has occurred.
MANIFEST – GMU1 software
mismatch, communication halted.

SYSTEM
OVERVIEW

GMU 44 Magnetometer

The GMU 44 has incorrect software installed. The G1000 system should be serviced.

Miscellaneous

FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

AUDIO PANEL
& CNS

190-00592-06 Rev. A

EIS

Message Advisory
Comments
FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is
is locked.
locked. This occurs when an aviation database update eliminates an obsolete
waypoint. The flight plan cannot find the specified waypoint and flags this message.
This can also occur with user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no longer exists in any database,
OR
update the waypoint name/identifier to reflect the new information.
FPL WPT MOVE – Flight plan
The system has detected that a waypoint coordinate has changed due to a new
waypoint moved.
aviation database update. Verify that stored flight plans contain correct waypoint
locations.
TIMER EXPIRD – Timer has expired.
The system notifies the pilot that the timer has expired.
DB CHANGE – Database changed.
This occurs when a stored flight plan contains procedures that have been manually
Verify user modified procedures.
edited. This alert is issued only after an aviation database update. Verify that the
user-modified procedures in stored flight plans are correct and up to date.
DB CHANGE – Database changed.
This occurs when a stored flight plan contains an airway that is no longer consistent
Verify stored airways.
with the aviation database. This alert is issued only after an aviation database update.
Verify use of airways in stored flight plans and reload airways as needed.
FPL TRUNC – Flight plan has been
This occurs when a newly installed aviation database eliminates an obsolete approach
truncated.
or arrival used by a stored flight plan. The obsolete procedure is removed from the
flight plan. Update flight plan with current arrival or approach.
LOCKED FPL – Cannot navigate
This occurs when the pilot attempts to activate a stored flight plan that contains
locked flight plan.
locked waypoint. Remove locked waypoint from flight plan. Update flight plan with
current waypoint.
WPT ARRIVAL – Arriving at waypoint
Arriving at waypoint [xxxx], where [xxxx] is the waypoint name.
-[xxxx]
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to turn.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the airspace.
ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within
than 10 minutes.
10 minutes.
ARSPC NEAR – Airspace near and
Special use airspace is near and ahead of the aircraft position.
ahead.
ARSPC NEAR – Airspace near – less
Special use airspace is within 2 nm of the aircraft position.
than 2 nm.
APR INACTV – Approach is not active. The system notifies the pilot that the loaded approach is not active. Activate
approach when required.

493

SYSTEM
OVERVIEW

Appendix A
Miscellaneous (Cont.)

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Message Advisory
SLCT FREQ – Select appropriate
frequency for approach.
SLCT NAV – Select NAV on CDI for
approach.
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach current
vertical waypoint.

FLIGHT
MANAGEMENT

VNV – Unavailable. Unsupported leg
type in flight plan.

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Parallel course
selected.
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
TRAFFIC FAIL – Traffic device has
failed.
STRMSCP FAIL – Stormscope has
failed.
FAILED PATH – A data path has
failed.
MAG VAR WARN – Large magnetic
variance. Verify all course angles.

Comments
The system notifies the pilot to load the approach frequency for the appropriate NAV
receiver. Select the correct frequency for the approach.
The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to
the correct NAV receiver.
Bad parallel track geometry.
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been passed.
The current vertical waypoint can not be reached within the maximum flight path
angle and vertical speed constraints. The system automatically transitions to the next
vertical waypoint.
The lateral flight plan contains a procedure turn, vector, or other unsupported leg
type prior to the active vertical waypoint. This prevents vertical guidance to the active
vertical waypoint.
The current crosstrack exceeds the limit, causing vertical deviation to go invalid.
The current track angle error exceeds the limit, causing the vertical deviation to go
invalid.
A parallel course has been selected, causing the vertical deviation to go invalid.
The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position
with alternate navigation sources.
The G1000 is no longer receiving data from the traffic system. The traffic device
should be serviced.
Stormscope has failed. The G1000 System should be serviced.
A data path connected to the GDU or the GIA 63/63W has failed.

INDEX

APPENDICES

The GDU’s internal model cannot determine the exact magnetic variance for
geographic locations near the magnetic poles. Displayed magnetic course angles may
differ from the actual magnetic heading by more than 2°.
SCHEDULER [#] – .
Message criteria entered by the user.
SVS – SVS DISABLED: Out of available Synthetic Vision is disabled because the aircraft is not within the boundaries of the
terrain region.
installed terrain database.
SVS – SVS DISABLED: Terrain DB
Synthetic Vision is disabled because a terrain database of sufficient resolution (9 arcresolution too low.
second or better) is not currently installed.

494

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Appendix A
SYSTEM
OVERVIEW

AFCS Status Annunciations

FLIGHT
INSTRUMENTS

The following annunciations (listed in order of increasing priority) can appear on the PFD above the
Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by
criticality.
AFCS Status Annunciation

EIS

Figure A-5 AFCS Status Annunciation

Aileron Mistrim Right
Aileron Mistrim Left

Elevator Mistrim Up
Pitch Trim Failure

Roll servo providing sustained force in the indicated direction

Pitch servo providing sustained force in the indicated direction
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move AP TRIM switches separately to unstick

Roll Failure

Roll axis control failure; AP inoperative

Pitch Failure

Pitch axis control failure; AP inoperative

System Failure

AP and MET are unavailable; FD may still be available
Performing preflight system test; aural alert sounds at completion
Do not press the AP DISC Switch during servo power-up and preflight system
tests as this may cause the preflight system test to fail or never to start (if
servos fail their power-up tests). Power must be cycled to the servos to remedy
the situation.

AFCS

Preflight Test

HAZARD
AVOIDANCE

(or stuck AP TRIM Switch)

Description

FLIGHT
MANAGEMENT

Elevator Mistrim Down

Annunciation

AUDIO PANEL
& CNS

Alert Condition

ADDITIONAL
FEATURES

Preflight system test failed; aural alert sounds at failure

APPENDICES
INDEX

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495

SYSTEM
OVERVIEW

Appendix A

SVS Terrain Alerts

FLIGHT
INSTRUMENTS

Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD. For more information
on SVS Terrain, refer to the Hazard Avoidance Section.
PFD/MFD
TERRAIN-SVS Page
Annunciation

Alert Type

Pop-Up Alert
(MFD Navigation Map
Page)

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Reduced Required Terrain
Clearance Warning (RTC)
Imminent Terrain Impact
Warning (ITI)
Reduced Required Obstacle
Clearance Warning (ROC)
Imminent Obstacle Impact
Warning (IOI)
Reduced Required Terrain
Clearance Caution (RTC)
Imminent Terrain Impact
Caution (ITI)
Reduced Required Obstacle
Clearance Caution (ROC)
Imminent Obstacle Impact
Caution (IOI)

Aural Message
“Warning; Terrain, Terrain”
“Warning; Terrain, Terrain”
“Warning; Obstacle, Obstacle”
“Warning; Obstacle, Obstacle”
“Caution; Terrain, Terrain”
“Caution; Terrain, Terrain”
“Caution; Obstacle, Obstacle”
“Caution; Obstacle, Obstacle”

AFCS

SVS Terrain Status Annunciations
PFD/MFD
TERRAIN-SVS Page
Annunciation

Alert Type

“Terrain System Failure”

ADDITIONAL
FEATURES

System Test Fail
Terrain Alerting is disabled

None

No GPS position or excessively
degraded GPS signal

“Terrain System Not Available”
None

System Test in progress

APPENDICES

Aural Message

None
None

“Terrain System Test OK”
“Terrain System Available”

INDEX

System Test pass
GPS signal is re-established

496

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190-00592-06 Rev. A

Appendix A
SYSTEM
OVERVIEW

Terrain Awareness and Warning System (TAWS) ALERTS
Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD. For more information
on TAWS, refer to the Hazard Avoidance Section.
Annunciation
(PFD/MFD
TAWS Page)

Pop-Up Alert
(MFD Navigation Map
Page)

Aural Message

“Caution, Terrain; Caution, Terrain”
or
“Terrain Ahead; Terrain Ahead”

“Terrain Ahead; Terrain Ahead”
or
“Caution, Terrain; Caution, Terrain”

“Caution, Obstacle; Caution, Obstacle”
or
“Obstacle Ahead; Obstacle Ahead”

“Obstacle Ahead; Obstacle Ahead”
or
“Caution, Obstacle; Caution, Obstacle”

Reduced Required
Terrain Clearance
Caution (RTC)
Imminent Terrain
Impact Caution (ITI)
Reduced Required
Obstacle Clearance
Caution (ROC)
Imminent Obstacle
Impact Caution (IOI)

Negative Climb Rate
Caution (NCR)

190-00592-06 Rev. A

“Too Low, Terrain”
None

None

“Five-Hundred”
“Sink Rate”

INDEX

Premature Descent
Alert Caution (PDA)
Altitude Callout “500”
Excessive Descent
Rate Caution (EDR)

APPENDICES

“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”

Imminent Obstacle
Impact Warning (IOI)

ADDITIONAL
FEATURES

“Obstacle, Obstacle; Pull Up, Pull Up”
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”

Reduced Required
Obstacle Clearance
Warning (ROC)

AFCS

Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”

HAZARD
AVOIDANCE

“Terrain, Terrain; Pull Up, Pull Up”
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”

FLIGHT
MANAGEMENT

Reduced Required
Terrain Clearance
Warning (RTC)

AUDIO PANEL
& CNS

“Pull Up”
EIS

Excessive Descent
Rate Warning (EDR)

Imminent Terrain
Impact Warning (ITI)

FLIGHT
INSTRUMENTS

Alert Type

“Don’t Sink”
or
“Too Low, Terrain”

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

497

SYSTEM
OVERVIEW

Appendix A
TAWS System Status Annunciations
Annunciation
(PFD/MFD TAWS
Page)

Pop-Up Alert
(MFD Navigation Map Page)

Aural Message

TAWS System Test Fail

None

“TAWS System Failure”

TAWS Alerting is disabled

None

No GPS position or excessively
degraded GPS signal

None

“TAWS Not Available”

System Test in progress

None

None
None

“TAWS System Test OK”
“TAWS Available”

EIS

FLIGHT
INSTRUMENTS

Alert Type

None
None

AUDIO PANEL
& CNS

System Test pass
GPS signal is re-established

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Annunciation

Figure A-6 TAWS Annunciation Locations

MFD

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

PFD

498

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Appendix B
SYSTEM
OVERVIEW

SD Card Use and Databases

FLIGHT
INSTRUMENTS

The G1000 System uses Secure Digital (SD) cards to load and store various types of data. For basic flight
operations, SD cards are required for database storage as well as Jeppesen aviation and ChartView database
updates.
CAUTION: Do not load Jeppesen navigation data (except ChartView) onto Garmin Supplemental Data

Cards.

Jeppesen Databases
EIS

The Jeppesen aviation database is updated on a 28-day cycle. The optional ChartView database is updated
on a 14-day cycle. If the ChartView database is not updated within 70 days of the expiration date, ChartView
no longer functions.

AUDIO PANEL
& CNS

Both these databases are provided directly from Jeppesen. The ChartView database should be copied to the
Garmin supplied Supplemental Data Card which resides in the bottom card slot on the MFD. The aviation
database must be installed from the Jeppesen or user supplied SD data card. Contact Jeppesen (www.jeppesen.
com) for subscription and update information.

FLIGHT
MANAGEMENT

NOTE: After the aviation database is installed, the card may be removed.

Updating the Jeppesen aviation database:

HAZARD
AVOIDANCE

1) With the G1000 System OFF, insert the SD card containing the aviation database update into the top card slot
of the PFD to be updated (label of SD card should face left).
2) Turn the G1000 System ON. A prompt similar to the following is displayed in the upper left corner of the PFD:

AFCS
ADDITIONAL
FEATURES

Figure B-1 Database Update Prompt

3) Press the ENT Key to start the database update. A prompt similar to the following is displayed:

APPENDICES
INDEX

Figure B-2 Database Update Confirmation

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499

SYSTEM
OVERVIEW

Appendix B
4) After the update completes, the PFD continues to power-up normally.
5) Turn the G1000 System OFF and remove the SD card.

FLIGHT
INSTRUMENTS

6) Repeat steps 1 through 4 for the MFD. The MFD and PFD databases are now updated. Remove the SD card
when finished.
7) Verify the correct update cycle is loaded during MFD power-up.

Garmin Databases

EIS

NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin

accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of
the data.

AUDIO PANEL
& CNS

• Expanded basemap –The basemap database contains data for the topography and land features, such as
rivers, lakes, and towns. It is updated only periodically, with no set schedule. There is no expiration date.

FLIGHT
MANAGEMENT

The following G1000 databases are stored on Supplemental Data Cards provided by Garmin:

• Airport terrain – The airport terrain database contains airport diagram data. It is updated periodically and
has no expiration date.

• Terrain – The terrain database contains terrain mapping data. It is updated periodically and has no expiration
date.

HAZARD
AVOIDANCE

• Obstacle – The obstacle database contains data for obstacles, such as towers, that pose a potential hazard to
aircraft. Obstacles 200 feet and higher are included in the obstacle database. It is very important to note that
not all obstacles are necessarily charted and therefore may not be contained in the obstacle database. This
database is updated on a 56-day cycle.

AFCS

• SafeTaxi – The SafeTaxi database contains detailed airport diagrams for selected airports. These diagrams aid
in following ground control instructions by accurately displaying the aircraft position on the map in relation
to taxiways, ramps, runways, terminals, and services. This database is updated on a 56-day cycle.

ADDITIONAL
FEATURES

• FliteCharts – The FliteCharts database contains procedure charts for the United States only. This database
is updated on a 28-day cycle. If not updated within 180 days of the expiration date, FliteCharts no longer
functions.

INDEX

APPENDICES

Since these databases are not stored internally in the PFD or MFD, a Supplemental Data Card containing
identical database versions must be kept in each display unit. After subscribing to the desired databases
product, these database products will be downloaded to two Supplemental Data Cards (with the exception of
FliteCharts, which is loaded on only one card). Insert each Supplemental Data Card into the correct location
shown in Figure B-3. If one of the Supplemental Data Cards contains the ChartView database, or the FliteCharts
database, this card must be inserted into the bottom card slot on the MFD. These cards must not be removed
except to update the databases stored on each card.

500

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190-00592-06 Rev. A

Appendix B
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS

MFD

EIS

PFD

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

Figure B-3 Correct Database Locations

HAZARD
AVOIDANCE

The Garmin database updates can be obtained by following the instructions detailed in the ‘Aviation Databases’
section of the Garmin website (www.garmin.com). Once the updated files have been downloaded from the
website, a PC equipped with an appropriate SD card reader is used to unpack and program the new databases
onto the existing Supplemental Data Cards. The following equipment is required to perform the update:
• Windows-compatible PC computer (Windows 2000 or XP recommended)
• SanDisk SD Card Reader, P/Ns SDDR-93 or SDDR-99 or equivalent card reader
• Updated database obtained from the Garmin website

AFCS

• Existing 010-00330-42 Supplemental Database SD Cards from both PFD and MFD

ADDITIONAL
FEATURES

In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database
product functional. It may also be necessary to have the system configured by a Garmin authorized service
facility in order to use some database features.
Updating Garmin databases:
1) Copy the data to the appropriate data cards.

APPENDICES

2) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of each PFD. The SD card
containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD.

INDEX

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501

SYSTEM
OVERVIEW

Appendix B

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

3) Apply power to the G1000 System. View the MFD power-up splash screen. Check that the databases are
initialized and displayed on the splash screen. When updating the terrain and FliteCharts databases, an ‘in
progress’ message may be seen. If this message is present, wait for the system to finish loading before verifying
the correct databases are initialized, then proceed to step 3.

FLIGHT
MANAGEMENT

Figure B-4 Database Information on the Splash Screen

4) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey.

5) Use the FMS Knob to select the AUX - System Setup Page.

HAZARD
AVOIDANCE

6) Select the DBASE Softkey to place the cursor in the ‘Database’ box.
7) Turn the FMS Knob to scroll through the list and check that all databases are current and there are no errors.

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

8) Power down the G1000.

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Appendix C
SYSTEM
OVERVIEW

Glossary

ADDITIONAL
FEATURES
APPENDICES
INDEX

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

AFCS

190-00592-06 Rev. A

barometric altitude
barometric setting
battery
backcourse

HAZARD
AVOIDANCE

B ALT
BARO
BATT
BC

FLIGHT
MANAGEMENT

ATK
AUTOSEQ
AUX
AWOS

The compass direction from the
present position to a destination
waypoint
BFO
beat frequency oscillator
BKSP
backspace
BRG
bearing
C
center runway
ºC
degrees Celsius
CA
Course to Altitude
CALC
calculator
Calibrated Airspeed Indicated airspeed corrected for
installation and instrument errors.
CD
Course to DME distance
CDI
Course Deviation Indicator
CDU
Control Display Unit
CF
Course to Fix
CHT
Cylinder Head Temperature
CHKLIST
checklist
CHNL
channel
CI
Course to Intercept
CLD
cloud
CLR
clear
cm
centimeter
CNS
Communication, Navigation, &
Surveillance
CO
carbon monoxide
COM
communication radio
CONFIG
configuration
COOL
coolant
COPLT
co-pilot
Course
The line between two points to be
followed by the aircraft
Course to Steer
The recommended direction to steer
in order to reduce course error or
stay on course. Provides the most
efficient heading to get back to the
desired course and proceed along
the flight plan
CR
Course to Radial
CRG
Cockpit Reference Guide
CRNT
current
Crosstrack Error
The distance the aircraft is off a
desired course in either direction, left
or right
CRS
course
CRS
Course to Steer
CRSR
cursor
CTA
Control Area
CTRL
control

AUDIO PANEL
& CNS

ATC
ATCRBS
ATIS

Bearing

EIS

AIM
AIRMET
ALRT
ALT
ALT, ALTN
AMPS
ANNUNC
ANT
AP
AP DISC
APR
APT
ARINC
ARSPC
ARTCC
ARV
AS
ASB
ASOS

accuracy
active, activate
air data computer
Automatic Direction Finder
Attitude Direction Indicator
Arc to fix
Automatic Flight Control System
Airplane Flight Manual
Airplane Flight Manual Supplement
airframe
Above Ground Level
Attitude and Heading Reference
System
Airman’s Information Manual
Airman’s Meteorological Information
alert
altitude
alternator
amperes
annunciation
antenna
autopilot
autopilot disconnect
approach
airport, aerodrome
Aeronautical Radio Incorporated
airspace
Air Route Traffic Control Center
arrival
airspeed
Aviation Support Branch
Automated Surface Observing
System
Air Traffic Control
ATC Radar Beacon System
Automatic Terminal Information
Service
along-track
automatic sequence
auxiliary
Automated Weather Observing
System

FLIGHT
INSTRUMENTS

ACC
ACT, ACTV
ADC
ADF
ADI
AF
AFCS
AFM
AFMS
AFRM
AGL
AHRS

503

SYSTEM
OVERVIEW

Appendix C

FLIGHT
INSTRUMENTS

Cumulative
CVR
CVRG
CWS
CYL

The total of all legs in a flight plan.
Cockpit Voice Recorder
coverage
control wheel steering
cylinder

density altitude
database
decibels ‘Z’ (radar return)
declutter
decrease fuel
degree
de-icing
departure
The desired course between the
active “from” and “to” waypoints
DEST
destination
DF
Direct to Fix
DFLT
default
DGRD
degrade
DH
decision height
Dilution of Precision A measure of GPS satellite geometry
quality on a scale of one to ten (lower
numbers equal better geometry,
where higher numbers equal poorer
geometry)
DIR
direction
DIS
distance
Distance
The ‘great circle’ distance from the
present position to a destination
waypoint
DME
Distance Measuring Equipment
DOP
Dilution of Precision
DP
Departure Procedure
DPRT
departure
DR
dead reckoning
DSBL
disabled
DTK
Desired Track

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

D ALT
DB, DBASE
dBZ
DCLTR, DECLTR
DEC FUEL
deg
DEIC, DEICE
DEP
Desired Track

APPENDICES

E
ECU
Efficiency

INDEX

EGT
EIS
ELEV
ELEV
EMERGCY
EMI
ENDUR

504

empty, east
Engine Control Unit
A measure of fuel consumption,
expressed in distance per unit of fuel
Exhaust Gas Temperature
Engine Indication System
elevation
elevator
emergency
Electromagnetic Interference
endurance

Endurance

Flight endurance, or total possible
flight time based on available fuel on
board
ENG
engine
ENGD
engaged
ENR
enroute
Enroute Safe Altitude The recommended minimum altitude
within ten miles left or right of the
desired course on an active flight
plan or direct-to
ENT
enter
EPE
Estimated Position Error
EPU
Estimated Position Uncertainty
ERR
error
ESA
Enroute Safe Altitude
Estimated Position Error A measure of horizontal GPS
position error derived by satellite
geometry conditions and other
factors
Estimated Time of Arrival The estimated time at which the
aircraft should reach the destination
waypoint, based upon current speed
and track
Estimated Time Enroute The estimated time it takes to
reach the destination waypoint from
the present position, based upon
current ground speed
ETA
Estimated Time of Arrival
ETE
Estimated Time Enroute
EXPIRD
expired
ºF
FA
FAA
FADEC
FAF
FAIL
FC
FCC
FCST
FD
FD
FDE
FFLOW
FIS-B
FISDL
FL
FLC
FM

degrees Fahrenheit
Course From Fix to Altitude
Federal Aviation Administration
Full Authority Digital Engine Control
Final Approach Fix
failure
Course From Fix to Distance
Federal Communication Commission
forecast
Course From Fix to DME Distance
flight director
Fault Detection and Exclusion
fuel flow
Flight Information ServicesBroadcast
Flight Information Service Data Link
flight level
Flight Level Change
Course From Fix to Manual
Termination

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix C

AFCS
ADDITIONAL
FEATURES
APPENDICES

key stuck
kilogram

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

190-00592-06 Rev. A

KEYSTK
kg

HAZARD
AVOIDANCE

Hold Terminating at Altitude
heading

Groundspeed

FLIGHT
MANAGEMENT

HA
HDG

GMA
GMT
GMU
GND
gph
GPS
Grid MORA

AUDIO PANEL
& CNS

Ground Track
GRS
GS
GTX

glideslope
go-around
gallon(s)
gearbox
Garmin Air Data Computer
Garmin Satellite Data Link
Garmin Display Unit
Garmin Engine/Airframe Unit
geographic
Garmin Flight Control
Garmin Integrated Avionics Unit
Global Navigation Satellite Landing
System
Garmin Audio Panel System
Greenwich Mean Time
Garmin Magnetometer Unit
ground
gallons per hour
Global Positioning System
Grid Minimum Off-Route Altitude;
one degree latitude by one degree
longitude in size and clears the
highest elevation reference point in
the grid by 1000 feet for all areas of
the grid
The velocity that the aircraft is
travelling relative to a ground
position
see Track
Garmin Reference System
Ground speed
Garmin Transponder

The direction an aircraft is pointed,
based upon indications from a
magnetic compass or a properly set
directional gyro
HF
Hold Terminating at Fix
HFOM
Horizontal Figure of Merit
Hg
mercury
HI
high
HI SENS
High Sensitivity
HM
Hold with Manual Termination
Horizontal Figure of Merit A measure of the uncertainty in
the aircraft’s horizontal position
hPa
hectopascal
HPL
Horizontal Protection Level
hr
hour
HSDB
High-Speed Data Bus
HSI
Horizontal Situation Indicator
HT
heat
HUL
Horizontal Uncertainty Level
Hz
Hertz
I
Inner Marker
IAF
Initial Approach Fix
IAT
Indicated Air Temperature
IAU
Integrated Avionics Unit
ICAO
International Civil Aviation
Organization
ICS
Intercom System
ID
Identification/Morse Code Identifier
IDENT, IDNT
identification
IF
Initial Fix
IFR
Instrument Flight Rules
IG
Imperial gallon
ILS
Instrument Landing System
IMC
Instrument
Meteorological
Conditions
in
inch
INACTV
inactive
INC FUEL
increase fuel
IND
indicated
Indicated
Information provided by properly
calibrated and set instrumentation
on the aircraft panel
INFO
information
in HG
inches of mercury
INT
intersection(s)
INTEG
integrity (RAIM unavailable)
IrDA, IRDA
Infrared Data Association

EIS

G/S, GS
GA
gal, gl
GBOX
GDC
GDL
GDU
GEA
GEO
GFC
GIA
GLS

Heading

FLIGHT
INSTRUMENTS

Fuel On Board

Flight Management System
Fuel On Board
flight plan
Flight Path Marker
feet per minute
frequency
freezing
Flight Service Station
foot/feet
The fuel flow rate, expressed in units
of fuel per hour
The total amount of usable fuel on
board the aircraft

SYSTEM
OVERVIEW

FMS
FOB
FPL
FPM
fpm
FREQ
FRZ
FSS
ft
Fuel Flow

505

SYSTEM
OVERVIEW

Appendix C
kHz
km
kt

kilohertz
kilometer
knot

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

L
left, left runway
LAT
latitude
LBL
label
lb
pound
LCD
Liquid Crystal Display
LCL
local
LED
Light Emitting Diode
Left Over Fuel On Board The amount of fuel remaining
on board after the completion of
one or more legs of a flight plan or
direct-to
Left Over Fuel Reserve The amount of flight time remaining,
based on the amount of fuel on
board after the completion of one or
more legs of a flight plan or directto, and a known consumption rate
Leg
The portion of a flight plan between
two waypoints
LIFR
Low Instrument Flight Rules
LNAV
Lateral Navigation
LO
low
LOC
localizer
LOI
loss of integrity (GPS)
LON
longitude
LPV
Localizer Performance with Vertical
guidance
LRU
Line Replacement Unit
LT
left
LTNG
lightning
LVL
level

APPENDICES

ADDITIONAL
FEATURES

M
m
MAG
MAG VAR
MAHP
MAN IN
MAN SQ
MAP
MASQ
MAX
MAXSPD
MDA

INDEX

MET
METAR

506

Middle Marker
meter
Magnetic
Magnetic Variation
Missed Approach Hold Point
manifold pressure (inches Hg)
Manual Squelch
Missed Approach Point
Master Avionics Squelch
maximum
maximum speed (overspeed)
barometric
minimum
descent
altitude
manual electric trim
Meteorological Aviation Routine

MEPT
manual electric pitch trim
MFD
Multi Function Display
MGRS
Military Grid Reference System
MHz
megahertz
MIC
microphone
MIN
minimum
Minimum Safe Altitude Uses Grid MORAs to determine
a safe altitude within ten miles of
the aircraft present position
MKR
marker beacon
MOA
Military Operations Area
MOV
movement
mpm
meters per minute
MSA
Minimum Safe Altitude
MSG
message
MSL
Mean Sea Level
MT
meter
mV
millivolt(s)
MVFR
Marginal Visual Flight Rules
N
NAV
NAVAID
NDB
NEXRAD
nm
NPT
NRST

north
navigation
NAVigation AID
Non-directional Beacon
Next Generation Radar
nautical mile(s)

O
OAT
OBS
OFST
OXY

Outer Marker
Outside Air Temperature
Omni Bearing Selector
offset
oxygen

P ALT
PA
PA
PASS
PC
PFD
PI
PIT, PTCH
POSN
PPM
P. POS
PRES, PRESS
PROC
psi
PT

pressure altitude
Passenger Address
Proximity Advisory
passenger(s)
personal computer
Primary Flight Display
Procedure Turn to Course Intercept
pitch
position
parts per million
Present Position
pressure
procedure(s), procedure turn
pounds per square inch
Procedure Turn

nearest

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Appendix C

RAM
REF
REM
REQ
RES
REV
RF
RMI
RMT
RNG
RNWY
ROL
ROM
rpm
RST FUEL
RSV
RT
RVRSNRY
RX

SID
SIGMET

190-00592-06 Rev. A

TRG
TRK
TRSA
TRUNC

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Sim
SLP/SKD

Track Angle Error

APPENDICES

SD
sec
SEL, SLCT
SFC
SIAP

TCA
TCAS
TEL
TEMP
TERM
TF
TFR
T HDG
TIS
TIT
TKE
TMA
TMR/REF
Topo
Track

ADDITIONAL
FEATURES

SCIT

south
Selective Availability
Static Air Temperature
Satellite-Based
Augmentation
System
Storm Cell Identification and
Tracking
Secure Digital
second(s)
select
surface
Standard Instrument Approach
Procedures
Standard Instrument Departure
Significant Meteorological
Information
simulator
slip/skid

true
Traffic Advisory
Tactical Air Navigation System
Terminal Aerodrome Forecast
True Airspeed
Traffic Advisory System
Total Air Temperature
Terrain Awareness and Warning
System
Terminal Control Area
Traffic Collision Avoidance System
telephone
temperature
terminal
Track Between Two Fixes
Temporary Flight Restriction
True Heading
Traffic Information System
Turbine Inlet Temperature
Track Angle Error
Terminal Maneuvering Area
Timer/Reference
topographic
Direction of aircraft movement
relative to a ground position; also
‘Ground Track’
The angle difference between the
desired track and the current track
target
track
Terminal Radar Service Area
truncated

AFCS

S
SA
SAT
SBAS

T
TA
TACAN
TAF
TAS
TAS
TAT
TAWS

HAZARD
AVOIDANCE

right, right runway
radial
Receiver Autonomous Integrity
Monitoring
random access memory
reference
remaining (fuel remaining)
required
reserve (fuel reserve entered by
pilot)
reverse, revision, revise
Constant Radius Turn to Fix
Radio Magnetic Indicator
remote
range
runway
roll
read only memory
revolutions per minute
reset fuel
reserve (fuel reserve entered by
pilot)
right
reversionary
receive

FLIGHT
MANAGEMENT

R
RAD
RAIM

AUDIO PANEL
& CNS

quantity

symbol
speed
Special Position Identification
speaker
squelch
service
stall
Standard Terminal Arrival Route
statistics
standby
standard
Stormscope
Special Use Airspace
suspend
Synthetic Vision System
software
system

EIS

QTY

SMBL
SPD
SPI
SPKR
SQ
SRVC, SVC
STAL
STAR
STATS
STBY
STD
STRMSCP
SUA
SUSP
SVS
SW
SYS

FLIGHT
INSTRUMENTS

parallel track
Push-to-Talk
power

SYSTEM
OVERVIEW

PTK
PTT
PWR

507

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Appendix C
TTL
TURN
TX

total
procedure turn
transmit

UNAVAIL
USR
UTC
UTM/UPS

unavailable
user
Coordinated Universal Time
Universal Transverse Mercator/
Universal Polar Stereographic Grid

VPL
VPROF
VPTH
VR
VS
VSI
VSR
VTF

Visual Meteorological Conditions
vertical navigation
volume
VHF Omni-directional Range
very high frequency omnidirectional
range station and tactical air
navigation
Vertical Protection Level
VNV profile, vertical profile
VNV path, vertical path
Heading Vector to Radial
vertical speed
Vertical Speed Indicator
Vertical Speed Required
vector to final

W
WAAS
WARN
WGS-84
WPT
WW
WX

watt(s), west
Wide Area Augmentation System
warning (GPS position error)
World Geodetic System - 1984
waypoint(s)
world wide
weather

XFER, XFR
XPDR
XTALK
XTK

transfer
transponder
cross-talk
cross-track

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

V, Vspeed
velocity (airspeed)
VA
Heading Vector to Altitude
VAPP
VOR approach
VAR
variation
VD
Heading Vector to DME Distance
Vdc
volts, direct current
VERT
vertical
Vertical Figure of Merit A measure of the uncertainty in
the aircraft’s vertical position
Vertical Speed Required The vertical speed necessary
to descend/climb from a current
position and altitude to a defined
target position and altitude, based
upon current groundspeed
VFOM
Vertical Figure of Merit
VFR
Visual Flight Rules
VHF
Very High Frequency
VI
Heading Vector to Intercept
VLOC
VOR/Localizer Receiver
VM
Heading Vector to Manual
Termination

VMC
VNAV, VNV
VOL
VOR
VORTAC

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Appendix D
SYSTEM
OVERVIEW

Frequently Asked Questions

FLIGHT
INSTRUMENTS

If a particular aspect of G1000 operational capability is not addressed by these commonly asked questions or in
the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized
dealer. Garmin is dedicated to supporting its products and customers.

What is WAAS?

EIS

The Wide Area Augmentation System (WAAS) uses a system of ground stations to correct any GPS signal
errors. These ground stations correct for errors caused by ionospheric disturbances, timing, and satellite
orbit errors. It also provides vital integrity information regarding the health of each GPS satellite. The signal
correction is then broadcast through one of two geostationary satellites. This correction information can then
be received by any WAAS-enabled GPS receiver.

AUDIO PANEL
& CNS

WAAS is designed to provide the additional accuracy, availability, and integrity necessary to enable users to
rely on GPS for all phases of flight. WAAS is currently available in the United States, including Alaska and
Hawaii.

How does WAAS affect approach operations?

FLIGHT
MANAGEMENT

Both LNAV/VNAV and LPV approaches use the accuracy of WAAS to include vertical (glide path) guidance
capability. The additional accuracy and vertical guidance capability allows improved instrument approaches to
an expanded number of airports throughout the U.S.

HAZARD
AVOIDANCE

The implementation of LPV approaches further improves precision approach capabilities. LPV approaches
are designed to make full use of the improved GPS signal from the WAAS. This approach combines the LNAV/
VNAV vertical accuracy with lateral guidance similar to the typical Instrument Landing System (ILS). LPV
approaches allow lower approach minimums.
If WAAS is not available for the final approach course, the approach downgrades, as indicated by the “Approach
downgraded. Use LNAV minima.” message.

AFCS

What is RAIM and how does it affect approach operations?
When WAAS is unavailable, the GPS receivers use Receiver Autonomous Integrity Monitoring (RAIM) to
perform the following functions:

ADDITIONAL
FEATURES

• Monitor and verify integrity and geometry of tracked GPS satellites
• Notify pilot when satellite conditions do not provide necessary coverage to support a certain phase of flight
• Predict satellite coverage of a destination area to determine whether the number of available satellites is
sufficient to satisfy requirements (refer to the System Overview Section for instructions on RAIM prediction)

APPENDICES

• Detect and exclude bad satellites from the navigation solution (Fault Detection and Exclusion, FDE)
RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection
limit (4.0 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches).
Without WAAS or RAIM, GPS position accuracy integrity cannot be monitored.

INDEX

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509

SYSTEM
OVERVIEW

Appendix D
Why might there be no approaches available for a flight plan?

FLIGHT
INSTRUMENTS

Approaches are available for the final destination airport in a flight plan or as a direct-to (keep in mind
that some VOR/VORTAC identifiers are similar to airport identifiers). If a destination airport does not have a
published approach, the G1000 indicates “NONE” for the available procedures.

What happens when an approach is selected? Can a flight plan with an approach, a departure, or an
arrival be stored?

EIS

When an approach, departure, or arrival is loaded into the active flight plan, a set of approach, departure,
or arrival waypoints is inserted into the flight plan, along with a header line showing the title of the selected
instrument procedure. The original enroute portion of the flight plan remains active, unless the instrument
procedure is activated. This may be done either when the procedure is loaded or at a later time.

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

Flight plans can also be stored with an approach, a departure, or an arrival. Note that the active flight plan
is erased when the system is turned off. Also, the active flight plan is overwritten when another flight plan is
activated. When storing flight plans with an approach, a departure, or an arrival, the G1000 uses the waypoint
information from the current database to define the waypoints. If the database is changed or updated, the
G1000 System automatically updates the information, provided the procedure has not been modified. Should
an approach, departure, or arrival procedure no longer be available, the flight plan becomes locked until the
procedure is deleted from the flight plan.

Can “slant Golf” (“/G”) be filed using the G1000?

HAZARD
AVOIDANCE

“/G” may be filed for a flight plan. The G1000 System meets the requirements of TSO-C129a with GIA 63 and
TSO-C146a with GIA 63W Class A1 or A2 installation. GPS approaches are not to be flown with an expired
database. See the approved Airplane Flight Manual (AFM) as well as the Aeronautical Information Manual
(AIM) for more information.

What does the OBS Softkey do?

Normal (OBS not activated)
• Automatic sequencing of waypoints

OBS
• Manual sequencing - ‘holds’ on selected
waypoint

• Manual course change on HSI not possible

• Manually select course to waypoint from
HSI

• Always navigates ‘TO’ the active waypoint

• Indicates ‘TO’ or ‘FROM’ waypoint

• Must be in this mode for final approach
course

• Cannot be set for final approach course or
published holding patterns

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

The OBS Softkey is used to select manual sequencing of waypoints. Activating OBS mode sets the current
active-to waypoint as the primary navigation reference and prevents the system from sequencing to the next
waypoint in a flight plan. When OBS mode is cancelled, automatic waypoint sequencing is continued, and
the G1000 automatically activates the next waypoint in the flight plan once the aircraft has crossed the present
active waypoint.

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Appendix D
SYSTEM
OVERVIEW

When OBS mode is active, the G1000 allows the pilot to set a desired course to/from a waypoint using the
CRS/BARO Knob and HSI (much like a VOR).

FLIGHT
INSTRUMENTS

The most common application for using the OBS Softkey is the missed approach. The G1000 suspends
automatic waypoint sequencing (indicated by a ‘SUSP’ annunciation placed on the HSI) when the missed
approach point (MAP) is crossed. This prevents the G1000 from automatically sequencing to the missed
approach holding point (MAHP). During this time, the OBS Softkey designation changes to SUSP. Selecting
the SUSP Softkey reactivates automatic waypoint sequencing. The OBS Softkey then resumes its normal
functionality.

Why might the G1000 not automatically sequence to the next waypoint?
EIS
AUDIO PANEL
& CNS

The G1000 only sequences flight plan waypoints when automatic sequencing is enabled (i.e., no ‘OBS’ or
‘SUSP’ annunciation on the HSI). For automatic sequencing to occur, the aircraft must also cross the bisector of
the turn being navigated. The bisector is a line passing through the waypoint common to two flight plan legs
at an equal angle from each leg.

How can a waypoint be skipped in an approach, a departure, or an arrival?

FLIGHT
MANAGEMENT

The G1000 allows the pilot to manually select any approach, departure, or arrival leg as the active leg of
the flight plan. This procedure is performed on the MFD from the Active Flight Plan Page by highlighting the
desired waypoint and selecting the ACT LEG Softkey then the ENT Key to approve the selection. The GPS
then provides navigation along the selected flight plan leg.

When does turn anticipation begin?

HAZARD
AVOIDANCE

The G1000 smooths adjacent leg transitions based on a normal 15° bank angle (with the ability to roll up to
30°) and provides three pilot cues for turn anticipation:
• A waypoint alert (‘Next DTK ###° in # seconds’ or ‘Next HDG ###° in # seconds’) appears on the PFD 10
seconds before the turn point and flashes as it counts down to zero.

AFCS

• A flashing turn advisory (‘Turn [right/left] to ###° in # seconds’) appears on the PFD 10 seconds before the
turn and flashes as it counts down to zero. ‘Turn [right/left] to ###° now’ or ‘Next [DTK/HDG] to ###° now’
is displayed when the pilot is to begin the turn and the HSI (GPS mode) automatically sequences to the next
DTK or HDG value.

ADDITIONAL
FEATURES

• The To/From indicator on the HSI flips momentarily to indicate that the midpoint of the turn has been
crossed.

When does the CDI scale change?

APPENDICES

Once a departure is activated, the G1000 Course Deviation Indicator (CDI) full scale deflection is set to 0.3
nm. The CDI scale changes to 1.0 nm (terminal mode) then ramps up to 2.0 nm (enroute mode) at 30 nm
from the departure airport. When 31 nm from the destination, the CDI scale smoothly transition from 2.0 nm
back to 1.0 nm (terminal mode). At 2.0 nm before the FAF during an active approach, the CDI scale transitions
down further based on the type of approach activated (LNAV, LNAV/VNAV, LPV). When a missed approach is
activated, the CDI is set to 0.3 nm. See the Flight Instruments Section for more details on CDI scaling.

INDEX

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511

SYSTEM
OVERVIEW

Appendix D
Why does the HSI not respond like a VOR when OBS mode is active?

FLIGHT
INSTRUMENTS

Unlike a VOR, the CDI scale used on GPS equipment is based on the crosstrack distance to the desired
course, not on the angular relationship to the destination. Therefore, the CDI deflection on the GPS is constant
regardless of the distance to the destination and does not become less sensitive when further away from the
destination.

What is the correct missed approach procedure? How is the missed approach holding point selected?

EIS

To comply with TSO specifications, the G1000 does not automatically sequence past the MAP. The first
waypoint in the missed approach procedure becomes the active waypoint when the SUSP Softkey is selected
after crossing the MAP. All published missed approach procedures must be followed, as indicated on the
approach plate.

AUDIO PANEL
& CNS

To execute the missed approach procedure prior to the MAP (not recommended), select the Active Flight Plan
Page and use the ACT LEG Softkey to activate the missed approach portion of the procedure.

FLIGHT
MANAGEMENT

After a missed approach, how can the same approach be re-selected? How can a new approach be
activated?
NOTE: Do not attempt to reactivate the current approach prior to crossing the missed approach point

(MAP). If an attempt to do so is made, an alert message “Are you sure you want to discontinue the current
approach?” appears. The G1000 directs the pilot back to the transition waypoint and does not take into
consideration any missed approach procedures, if the current approach is reactivated.

HAZARD
AVOIDANCE

After flying the missed approach procedure, the pilot may reactivate the same approach for another attempt by
pressing the PROC Key. Once the clearance is given for another attempt, activate the approach by highlighting
‘Activate Approach’ using the large FMS Knob and pressing the ENT Key. The G1000 provides navigation
along the desired course to the waypoint and rejoins the approach in sequence from that point.

AFCS

To activate a new approach for the same airport, select the new procedure by pressing the PROC Key. Choose
‘Select Approach’, select the desired approach from the list shown, and press the ENT Key. Select the
desired transition, then activate the approach using the ENT Key.

INDEX

APPENDICES

ADDITIONAL
FEATURES

To activate a new approach to a different airport, press the Direct-to Key and select the desired airport using
the FMS Knobs. Press the ENT Key to accept the selected airport, then follow the steps in the preceding
paragraph to select an approach for the new airport.

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Appendix E
SYSTEM
OVERVIEW

General TIS Information

FLIGHT
INSTRUMENTS

NOTE: Aircraft without an operating transponder are invisible to TIS.
NOTE: TIS is not intended to be used as a collision avoidance system and does not relieve the pilot of the

responsibility to “see and avoid” other aircraft. TIS should not be used for avoidance maneuvers during
instrument meteorological conditions (IMC) or when there is no visual contact with the intruder aircraft.

EIS

The Traffic Information Service (TIS) provides traffic advisory information to non-TAS/TCAS-equipped aircraft.
TIS is a ground-based service providing the relative locations of all ATCRBS Mode-A and Mode-C transponder
equipped aircraft within a specified service volume. The TIS ground sensor uses real-time track reports to generate
traffic notification. The G1000 System displays TIS traffic information on the Traffic Map Page of the MFD. TIS
information may also be displayed for overlay on the MFD Navigation Map Page, as well as on the PFD Inset
Map. Surveillance data includes all transponder-equipped aircraft within the coverage volume. The G1000
System displays up to eight traffic targets within a 7.5-nm radius, from 3,000 feet below, to 3,500 feet above the
requesting aircraft.

AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT

The main difference between the Traffic Information System (TIS) and Traffic Advisory (TAS) or Traffic Collision
Avoidance Systems (TCAS) is the source of surveillance data. TAS/TCAS uses an airborne interrogator with a halfsecond update rate, while TIS utilizes the terminal Mode-S ground interrogator and accompanying data link to
provide a five-second update rate. TIS and TAS/TCAS have similar ranges.

HAZARD
AVOIDANCE

TIS relies on surveillance of the Mode-S radar system, which is a “secondary surveillance” radar system similar
to that used by ATCRBS. Many limitations are inherent in secondary radar surveillance. Information provided by
TIS is neither better nor more accurate than the information used by ATC. TIS is intended only to assist in visual
acquisition of other aircraft in visual meteorological conditions (VMC). While TIS is a useful aid for visual traffic
avoidance, system limitations must be considered to ensure proper use. No recommended avoidance maneuvers
are given, nor authorized, as a direct result of a TIS intruder display or TIS advisory.

AFCS

• TIS operation may be intermittent during turns or other maneuvering.

ADDITIONAL
FEATURES

• TIS is dependent on two-way, line-of-sight communications between the aircraft and the Mode-S radar antenna.
Whenever the structure of the aircraft comes between the transponder antenna and the ground-based radar
antenna, the signal may be temporarily interrupted.
Note: Refer to the TIS Limitations section of the Aeronautical Information Manual (AIM) for a more

comprehensive explanation of limitations and anomalies associated with TIS.

APPENDICES

NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in

mountainous regions.

INDEX

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513

SYSTEM
OVERVIEW

Appendix E

WARNING: Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations

is the responsibility of the FAA. Refer to the AIM for a Terminal Mode S radar site map.

EIS

FLIGHT
INSTRUMENTS

TIS information is collected during a single radar sweep. Collected information is then sent through the Mode
S uplink on the next radar sweep. Because of this, the surveillance information is approximately five seconds old.
TIS ground station tracking software uses prediction algorithms to compensate for this delay. These algorithms
use track history data to calculate expected intruder positions consistent with the time of display. Occasionally,
aircraft maneuvering may cause variations in this calculation and create slight errors on the Traffic Map Page which
affect relative bearing information and the target track vector and may delay display of the intruder information.
However, intruder distance and altitude typically remain relatively accurate and may be used to assist in spotting
traffic. The following errors are common examples:

AUDIO PANEL
& CNS

• When the client or intruder aircraft maneuvers excessively or abruptly, the tracking algorithm may report
incorrect horizontal position until the maneuvering aircraft stabilizes.
• When a rapidly closing intruder is on a course that intercepts the client aircraft course at a shallow angle
(either overtaking or head-on) and either aircraft abruptly changes course within 0.25 nm, TIS may display the
intruder aircraft on the incorrect side of the client aircraft.

FLIGHT
MANAGEMENT

These are rare occurrences and are typically resolved within a few radar sweeps once the client/intruder aircraft
course stabilizes.

HAZARD
AVOIDANCE

Pilots using TIS can provide valuable assistance in the correction of malfunctions by reporting observations
of undesirable performance. Reports should identify the time of observation, location, type and identity of the
aircraft, and describe the condition observed. Reports should also include the type of transponder and transponder
software version. Since TIS performance is monitored by maintenance personnel, not ATC, malfunctions should
be reported in the following ways:
• By telephone to the nearest Flight Service Station (FSS) facility

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

• By FAA Form 8000-7, Safety Improvement Report (postage-paid card can be obtained at FAA FSSs, General
Aviation District Offices, Flight Standards District Offices, and General Aviation Fixed Base Operators)

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Appendix F
SYSTEM
OVERVIEW

Map Symbols
Airports

Basemap
Item

Symbol

Unknown Airport

Interstate Highway

Non-towered, Non-serviced Airport

State Highway

FLIGHT
INSTRUMENTS

Item

Symbol

EIS

US Highway

Towered, Non-serviced Airport

National Highway

Non-towered, Serviced Airport

AUDIO PANEL
& CNS

City
Towered, Serviced Airport
State/Province Border
Restricted (Private) Airport
Heliport

FLIGHT
MANAGEMENT

International Border
Road
Railroad

NAVAIDS
Symbol

HAZARD
AVOIDANCE

Item

Latitude/Longitude

Intersection
LOM (compass locator at outer marker)

Airspace Boundaries

Mode C Tower Area

VOR/ILS
VORTAC

Warning Area Prohibited Area
Alert Area
Restricted Area
Caution Area Training Area
Danger Area
Unknown Area
Class C
Terminal Radar Service Area
Mode C Area

APPENDICES

TACAN

ADDITIONAL
FEATURES

VOR/DME

Symbol

AFCS

VOR

Item
ICAO Control Area
Class B Airspace

NDB (non-directional radio beacon)

Military Operations Area (MOA)
INDEX

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515

SYSTEM
OVERVIEW

Appendix F
Hazard Avoidance Features

FLIGHT
INSTRUMENTS

Feature

Symbol

Item

Terrain Proximity/TAWS display enabled

Non-threat Traffic

Traffic display enabled

Proximity Advisory (not used with TIS)

NEXRAD display enabled

Traffic Advisory, Out of Range

Cloud Top display enabled

EIS

Traffic
Symbol

Traffic Advisory

AUDIO PANEL
& CNS

Echo Top display enabled

Miscellaneous

XM Lightning display enabled

Item
Cell Movement display enabled

FLIGHT
MANAGEMENT

SIGMETs/AIRMETs display enabled
METARs display enabled

HAZARD
AVOIDANCE

Surface Analysis display enabled

ADDITIONAL
FEATURES

AFCS

Freezing Levels display enabled

APPENDICES

ARTCC Frequency or FSS Frequency
Map Pointer (when panning)
Elevation Pointer
(on Topography Scale when panning)

City Forecast display enabled

Measuring Pointer
Wind Vector

Winds Aloft display enabled

Overzoom Indicator

County Warnings display enabled

User Waypoint

Cyclone Warnings display enabled

Vertical Navigation Along Track Waypoint

Loss of hazard avoidance feature
(loss of GPS position)

Parallel Track Waypoint

Turbulence

Unanchored Flight Path Waypoint

Icing Potential
PIREPs

Symbol

Top of Descent (TOD)
Bottom of Descent (BOD)

INDEX

AIREPs
Navigating using Dead Reckoning

516

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Appendix F
SYSTEM
OVERVIEW

Obstacle Database
Unlighted Obstacle
Lighted Obstacle
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL

Obstacle Location
FLIGHT
INSTRUMENTS

Red obstacle is above or within 100 ft
below the aircraft altitude
Yellow obstacle is between 100 ft and
1000 ft below the aircraft altitude

EIS

Gray obstacle is more than 1000 ft
below aircraft altitude

AUDIO PANEL
& CNS

Table F-1 Obstacle Colors

Terrain Avoidance Colors and Symbols

FLIGHT
MANAGEMENT

Terrain Above Aircraft Altitude
Aircraft Altitude

100 ft Threshold

Red terrain is above
or within 100 ft below
the aircraft altitude

HAZARD
AVOIDANCE

1000 ft
Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude

Black terrain is more than 1000 ft below the aircraft altitude

AFCS

Figure F-1 Terrain Altitude/Color Correlation

ADDITIONAL
FEATURES

Figure F-2 TAWS Potential Impact Points

APPENDICES
INDEX

190-00592-06 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

517

INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Appendix F

Blank Page

518

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Index

EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE

B
Backlighting-------------------------------------------------- 41
Barometric altimeter setting---------------------------44, 50
Bearing/distance, measuring------------------------------143
Bearing information----------------------------------------- 57
Bearing Information Windows----------------------------- 45
Bearing pointer----------------------------------------------- 56
Bearing source----------------------------------------------- 57
Bus voltage--------------------------------------------------- 88

AFCS
ADDITIONAL
FEATURES

C
Calibrated Airspeed-----------------------------------------239
CDI---------------------------------- 233, 247, 258, 266, 273
CELL MOV Softkey------------------------------------------293
Chart Not Available---------------------------------- 424, 445
Chart options----------------------------------------- 432, 452
Chart setup box-------------------------------------- 438, 456
ChartView---------------------------------403, 423, 442, 444
ChartView database--------------------------- 440, 442, 443
ChartView functions----------------------------------------423
ChartView plan view---------------------------------------433
ChartView profile view-------------------------------------434
ChartView softkeys-----------------------------------------423
ChartView subscription------------------------------------442

INDEX

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

APPENDICES

190-00592-06 Rev. A

Approach box-----------------------------------------------447
Approach Mode, AFCS------------------------ 384, 397, 398
APR softkey------------------------------------------- 236, 242
Arrival procedure-189, 203, 231, 233, 234, 236, 256, 258,
267
Assist, engine leaning---------------------------------- 83–85
Attitude and Heading Reference System (AHRS)----- 3, 8,
13–14
Attitude indicator-------------------------------------------- 44
Audio alerting system--------------------------------------480
Audio Panel------------------------------------------------ 2, 10
Audio panel controls
SPKR-------------------------------------------------------124
Audio panel fail-safe operation---------------------------130
Automatic Flight Control System (AFCS)------ 1, 357–402
Controls-------------------------------------------- 358–359
Example procedures------------------------------ 388–395
Status Annunciations------------------------------------401
Status Box-------------------------------------------------361
Automatic squelch------------------------------------------104
Autopilot----------------------------------------357, 386–387
Disconnect----------------------------------- 359, 378, 387
Auto-tuning--------------------------------------------------112
Auto-tuning, COM------------------------------------------- 99
Auto-tuning, NAV-------------------------------------------108
Auto Zoom---------------------------------------------------136
Auxiliary Pages (AUX)--------------------------------------- 31
AUX - system status page-442, 443, 444, 460, 461, 463
Aviation Symbols------------------------------------- 148, 149

FLIGHT
INSTRUMENTS

Activate a Flight Plan---------------------------------------208
Active channel-----------------------------------------------464
Active frequency--------------------------------------- 96, 105
ADF---------------------------------------------------------114
ADF
ADF mode------------------------------------------ 114, 116
ANT mode-------------------------------------------------116
Volume-----------------------------------------------------114
ADF/BFO-----------------------------------------------------116
ADF/DME tuning--------------------------------------------117
ADF volume--------------------------------------------------116
AHRS--------------------------------------------------- 492, 493
Air Data Computer (ADC)------------------------------------ 3
AIRMETs------------------------------------------------------294
Airport
Information-----------------------------------------------166
Airspace Alerts--------------------------------------- 181, 182
Airspeed indicator---------------------------------------44, 46
Airspeed Reference-----------------------------------------368
Airspeed Trend Vector--------------------------------------- 46
Airways
Collapsed--------------------------------------------------221
Expanded--------------------------------------------------221
Alerting system----------------------------------------------479
Alert levels---------------------------------------------------480
Alerts---------------------------------------------------------479
Aircraft-----------------------------------------------------481
Audio voice-----------------------------------------------482
Alerts window------------------------------------------------ 69
Along Track Offset----------------------------------- 212, 213
ALT------------------------------------------------------------271
Altimeter--------------------------------------------------44, 49
Altitude
Constraints----------------------------------------- 224, 258
Altitude alerting---------------------------------------------- 72
Altitude capture-------------------------------------- 365, 374
Altitude Hold Mode (ALT)----------------------------------366
Altitude Reference----------------------------- 365, 366, 374
Ammeter------------------------------------------------------ 88
Annunciations
AFCS Status-----------------------------------------------495
G1000 System-------------------------------- 10, 483–484
TAWS Status----------------------------------------------498
Test tone---------------------------------------------- 12, 480
Annunciation Window-------------------------------------- 45
Annunciator lights------------------------------------------124
ANT/BFO-----------------------------------------------------116
Approach-----------------------------------------------------510
Activating-------------------------------------------------237
ILS----------------------------------------------------------397
Loading--------------------------------------- 205, 234, 236
Missed-----------------------------------------------------399
Removing--------------------------------------------------237

SYSTEM
OVERVIEW

I-1

SYSTEM
OVERVIEW

Index

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

FLIGHT
INSTRUMENTS

Checklists--------------------------------------------- 469–470
Checklist softkeys-------------------------------------------469
CLD TOP Softkey--------------------------------------------291
Closest Point-------------------------------------------------221
COM channel spacing--------------------------------------103
COM frequency box-------------------------------------93, 96
Command Bars, flight director----------------------------362
Communication (COM) frequency box------------------- 44
COM tuning failure-----------------------------------------130
Controls
AFCS------------------------------------------------ 358–359
PFD/MFD------------------------------------------18–19, 28
Softkeys------------------------------------------------ 20–23
Control Wheel Steering (CWS)--------------------- 359, 387
Copy a Flight Plan------------------------------------------208
County Warnings--------------------------------------------304
Course Deviation Indicator (CDI)--------------------- 58–59
Changing scale-------------------------------------------511
Course To Altitude------------------------------------------238
Cyclone-------------------------------------------------------305
Cylinder Head Temperature (CHT °F)--------------------- 78

INDEX

APPENDICES

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

Databases-----------------------------------------7, 8, 12, 499
Data entry------------------------------------------------ 27–28
Data Link Receiver--------------------------------------------- 4
Datalink receiver troubleshooting------------------------476
Data logging-------------------------------------------------473
Date and time------------------------------------------------ 34
Day/Night views-------------------------------------- 438, 456
Day view----------------------------------438, 439, 456, 457
Dead Reckoning---------------------------------------------- 74
DEC FUEL softkey-------------------------------------------- 82
Decision Height (DH)------------------------------------45, 73
Declutter, display--------------------------------------------- 75
Declutter maps-------------------------------------------21, 26
Delete Flight Plans------------------------------------------209
Deleting
An entire airway----------------------------------- 210, 211
An entire procedure------------------------------ 210, 211
An individual waypoint--------------------------- 210, 211
Flight Plan Items-----------------------------------------210
Density Altitude---------------------------------------------241
Departure
Procedure------------------------------201, 216, 228, 230
Select------------------------------------228, 231, 234, 237
Time--------------------------------------------------------239
Timer-------------------------------------------------------- 40
Dilution of Precision (DOP)--------------------------------- 17
Direct-to-- 160, 183, 184, 185, 186, 187, 222, 223, 256,
258, 273
Display backup-------------------------------------------10, 95
Display controls----------------------------------------- 18–25
DME

I-2

HOLD mode-----------------------------------------------117
NAV1 mode-----------------------------------------------117
NAV2 mode-----------------------------------------------117
Tuning mode--------------------------------------- 114, 117
DME information-----------------------------------------56, 57
DR mode------------------------------------------------------ 74

E
ECHO TOP Softkey------------------------------------------290
Electronic checklists-------------------- 403–404, 469, 470
Emergency checklist----------------------------------------471
Emergency frequency---------------------------------------130
Endurance, calculated (ENDUR)-----------------------80, 82
Engine Airframe Unit------------------------------------------ 3
Engine Indication System (EIS)------------------------ 77–90
Engine Manifold Pressure (MAN IN HG)--- 78, 80, 86, 88
Entertainment inputs---------------------------------------128
Estimated Position Error (EPE)----------------------------- 17
Exhaust Gas Temperature (EGT)---------------------- 83–84

F
Fail-safe operation------------------------------------------130
Field of View (SVS)------------------------------------------159
Flight data---------------------------------------------------472
Flight director-----------------------------------357, 360–361
Pitch modes---------------------------------------- 363–369
Roll modes------------------------------------------------379
Flight Level Change Mode (FLC)------------------ 368, 393
Flight plan
Closest point to reference------------------------------221
Storing-----------------------------------------------------510
Flight timer---------------------------------------------------- 39
FliteCharts------------------------- 444, 446, 458, 461, 500
FliteCharts database---------------------------------------460
FliteCharts functions---------------------------------------444
FPA----------------------------------------------------- 224, 263
Freezing Levels--------------------------------------- 297, 298
Frequency
Nearest----------------------------------------------------179
Frequency spacing------------------------------------------103
Frequency transfer arrow----------------------------------- 97
Frequently asked questions--------------------------------509
Fuel
Calculations------------------------------------------------ 82
Efficiency--------------------------------------------------241
Endurance-------------------------------------------------241
Flow--------------------------------------------------------- 81
Quantity---------------------------------------------------- 80
Remaining-------------------------------------------------241
Required---------------------------------------------------241
Statistics---------------------------------------------------241
Fuel calculations--------------------------------------------- 88
Fuel Flow (FFLOW GPH)--------------------------- 78, 86, 88
Fuel on Board-----------------------------------------------241

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Index

190-00592-06 Rev. A

O
OBS Mode-------------------------------------------63, 63–64
Obstacles---------------------------------------------- 487, 490
Oil Pressure (OIL PSI)------------------------------------78, 80
Oil Temperature (OIL °F)------------------------------------ 78
Omni Bearing Selector (OBS)----------------------- 510–511

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

Land Symbols------------------------------------------------147
Line Replaceable Units (LRU)------------------------ 2–5, 11
LNAV----------------------------------------------------------247
LO SENS------------------------------------------------------113
Low Altitude Annunciation--------------------------------- 72
LPV----------------------------------------------------- 247, 273
LPV approach------------------------------------------------388

APPENDICES

Jeppesen aviation database-------------------------------499

ADDITIONAL
FEATURES

National Weather Service----------------------------------304
NAV frequency box------------------------------------------ 93
Navigation
Database------------------------------------------- 224, 225
Map--------------------------------------------------------186
Navigation Mode, AFCS---------------- 382–383, 391–392
Navigation mode selection--------------------------------105
Navigation (NAV) frequency box-------------------------- 44
Navigation source-------------------------------------- 58–59
Navigation status box--------------------------------------- 44
Nav radio selection-----------------------------------------105
NAV tuning knob-------------------------------------------107
Nearest
Airport-------------- 163, 164, 165, 166, 179–182, 236
Airport Minimum Runway Length---------------------166
Airports Page-------------------------------- 164, 165, 166
Airport Surface Matching-------------------------------166
VOR------------------------------------------------- 179–180
Nearest Pages (NRST)--------------------------------------- 31
NEXRAD Softkey--------------------------------------------286
Night view--------------------------------438, 439, 456, 457
Non-path descent------------------------------373, 395–396
Normal display operation------------------------------------- 9

AFCS

ID indicator--------------------------------------------------107
ILS approach-------------------------------------------------397
Indicated airspeed------------------------------------------- 46
Indicated Altitude-------------------------------------------239
INFO box-----------------------------------------------------448
Inset Map, PFD----------------------------------------------- 45
Integrated Avionics Unit (IAU)------------------------------- 2
Intercom system (ICS)--------------------------------------128
Intersection
Information---------------------------------------- 167–168
Inverting a flight plan--------------------------------------208
IOI------------------------------------------------------ 323, 332

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

Heading------------------------------------------------------- 44
Heading bug-------------------------------------------------- 44
Heading Select Mode (HDG)----------------------- 381, 389
HI SENS-------------------------------------------------------113
Horizontal situation indicator--------------------------44, 53
HSI double green arrow------------------------------------105
HSI magenta arrow-----------------------------------------105
HSI single green arrow-------------------------------------105

AUDIO PANEL
& CNS

Manual Electric Trim (MET)------------------------- 357, 386
Map
Panning----------------------------------------------------138
Map Pages (MAP)------------------------------------------- 30
Map symbols------------------------------------------------515
Marker beacon----------------------------------------------113
Marker beacon annunciations----------------------------- 70
MASQ processing-------------------------------------------- 91
Measurement units, changing displayed----------------- 35
Menus--------------------------------------------------------- 27
Message advisories-- 481, 485, 486, 487, 491, 492, 493,
494
METARs------------------------------------------------------295
Minimum Descent Altitude (MDA)--------------------45, 73
Missed Approach----------- 189, 238, 243, 247, 273, 399
Mode S------------------------------------------------ 118, 119
Morse code identifier---------------------------------------107
Multi Function Display (MFD)-------------------------------- 2
Controls----------------------------------------------- 18–19
Softkeys----------------------------------------------------- 25

EIS

GDL 69/69A-------------------------------------------------277
GFC 700 AFCS--------------------------------------- 357–402
Glidepath-----------------------------------------------------271
Glidepath indicator------------------------------------------ 52
Glidepath Mode (GP)-------------------------- 375, 384, 398
Glideslope----------------------------------------------------271
Glideslope indicator----------------------------------------- 52
Glideslope Mode (GS)------------------------------- 377, 397
Global Positioning System (GPS)
Navigation----------------------------------------- 183–276
Go Around Mode (GA)----------------- 359, 378, 399–400
GTX 33 Transponder----------------------------------------118

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Fuel Quantity (FUEL QTY GAL)----------------------------- 78
Fuel remaining (GAL REM)--------------------------------- 88
Fuel used (GAL USED)--------------------------------------- 88

I-3

SYSTEM
OVERVIEW

Index
Other Statistics--------------------------------------- 239, 241
Outside Air Temperature (OAT)------------------------44, 65
Overspeed protection, autopilot--------------------------402

FLIGHT
INSTRUMENTS

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS

EIS

Page groups--------------------------------------------- 29–32
Page menus--------------------------------------------------- 27
Parallel Track------------------------------------------ 214, 216
Passenger address------------------------------------------127
PA system----------------------------------------------------127
Pilot profiles--------------------------------------------- 36–37
Pitch Hold Mode (PIT)--------------------------------------364
Pitch modes, flight director------------------------- 363–369
Pitch Reference----------------------------------------------364
Power-up page--------------------------------- 440, 459, 469
Power-up, system---------------------------------------------- 8
Primary Flight Display (PFD)---------------------------------- 2
Controls----------------------------------------------- 18–19
Softkeys------------------------------------------------ 20–22
Procedure examples, AFCS------------------------- 388–400
Procedure Loading Pages (PROC)------------------------- 32

Q
Quick tuning 121.500 MHz-------------------------------- 98

ADDITIONAL
FEATURES

AFCS

HAZARD
AVOIDANCE

RAIM--------------------- 16, 233, 243, 244, 245, 246, 509
Range---------------------------------------------------------157
Receiver Autonomous Integrity Monitoring--------- 16–17
Receiver Autonomous Integrity Monitoring (RAIM)---243
Required
Vertical Speed--------------------------------------------264
Vertical Speed Indicator---------------------------------264
Reversionary mode-----------------------------------------130
Reversionary Mode--------------------------------------- 9–10
ROC---------------------------------------------------- 323, 332
Roll Hold Mode (ROL)--------------------------------------380
Roll modes, flight director-------------------------- 379–382
Roll Reference-----------------------------------------------380
RVSI---------------------------------------------------- 264, 265
RX indicator--------------------------------------------------- 97

INDEX

APPENDICES

SafeTaxi------------------------------------403, 417, 420, 500
SafeTaxi database-------------------------------------------421
SBAS--------------------------------------------- 243, 245, 246
Scheduler---------------------------------------------- 467, 471
Secure Digital (SD) card-------------------- 7, 469, 472, 499
Selected Altitude--------------44, 365, 367, 370, 374, 389
Selected Altitude Bug--------------------------------------- 44
Selected Altitude Capture Mode-------365, 366, 367, 370
Selected Course----------------------------- 45, 54, 383, 385
Selected Heading--------------------------------- 45, 54, 381

I-4

Selecting a COM radio-------------------------------------- 96
Sequencing, automatic-------------------------------------511
Service Class-------------------------------------------------463
Servos------------------------------------------------------4, 386
SIGMETs------------------------------------------------------294
Slip/Skid Indicator----------------------------------------44, 48
Softkeys------------------------------------------------------- 44
EIS-------------------------------------------------------25, 80
LTNG-------------------------------------------------------292
MFD--------------------------------------------------------- 25
PFD----------------------------------------------------- 20–22
Sort Flight Plans---------------------------------------------208
Speaker-------------------------------------------------------124
Splash screen, power-up-------------------------------------- 8
Standby frequency-------------------------------- 96, 99, 105
ADF---------------------------------------------------------114
Standby frequency field------------------------------------- 96
Stereo headsets---------------------------------------------124
Stormscope--------------------------------------------------306
Stuck microphone-------------------------------------------130
Sunrise--------------------------------------------------------240
Sunset--------------------------------------------------------240
Surface Analysis---------------------------------------------297
SVS troubleshooting----------------------------------------474
Symbols, map------------------------------------------------515
Synthetic vision (SVS)------------------------------- 403, 404
System annunciations--------------------------------- 10, 479
System Page (EIS)-------------------------------------------- 88
System power-up---------------------------------------------- 8
System time--------------------------------------------------- 44

T
Tachometer (RPM)----------------------------- 78, 81, 86, 88
TAFs-----------------------------------------------------------295
TAS------------------------------------------------------------492
TAWS--------------------------------------321, 330, 497, 498
Terminal procedures charts------------------------- 424, 445
Terrain--------------------------------------------------------487
Color indications-----------------------------------------517
Terrain Awareness and Warning System (TAWS)-- 71, 497
Terrain Proximity--------------------------------------------311
Terrain-SVS---------------------------------------------------316
Timer
Departure--------------------------------------------------- 40
Flight-------------------------------------------------------- 39
Timer, PFD generic------------------------------------------- 38
TIS-------------------------------------------------------------339
TOD---------------------------------------------- 263, 264, 270
TOPO DATA------------------------------------- 144, 145, 154
Top of Descent--------------------------------------- 263, 264
TOPO SCALE-------------------------------------------------146
Total flight hours-----------------------------------------80, 88
Track indicator------------------------------------------------ 44
Track Vector--------------------------------------------------155

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Index

HAZARD
AVOIDANCE

XM
Radio------------------------------------------------ 277, 462
Receiver troubleshooting-------------------------------476
Satellite Weather-----------------------------------------277
Activating-------------------------------------------------278
XM channel list----------------------------------------------464
XM presets---------------------------------------------------466
XM radio-----------------------------------------------------464
XM radio entertainment-----------------------------------128
XM radio volume--------------------------------------------466
XM satellite radio------------------------------------ 462, 464
XM Satellite Radio--------------------------------------------- 4
XM Satellite Weather
AIREPs-----------------------------------------------------302
Icing--------------------------------------------------------300
PIREPs-----------------------------------------------------302
Turbulence-------------------------------------------------301

AFCS
ADDITIONAL
FEATURES
APPENDICES

Z
Zoom
Auto--------------------------------------------------------136

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

INDEX

190-00592-06 Rev. A

WAAS-------------------------------------------- 247, 388, 490
Warranty--------------------------------------------------------- i
Waypoint
Automatic sequencing--------------------------- 510, 511
Skipping---------------------------------------------------511
Waypoint Pages (WPT)-------------------------------------- 30
Waypoint Selection Submenu--- 184, 191, 194, 196, 243
Wind--------------------------------------------------- 134, 156
Wind data----------------------------------------------------- 45
Winds Aloft--------------------------------------------------299
WIND Softkey------------------------------------------------299

FLIGHT
MANAGEMENT

VDI----------------------------------------------------- 264, 265
Vertical deviation-------------------------------------------372
Vertical deviation guidance-------------------------------225
Vertical Deviation Indicator-------------------------------264
Vertical Deviation Indicator (VDI)-------------------------- 52
Vertical navigation------------------------------------------224
Direct-to---------------------------------------------------223
Vertical Navigation (VNV)
Flight control--------------------------------------- 370–374
Vertical Path Tracking Mode (VPTH)--------370–371, 394
Vertical speed guidance-----------------------------------225
Vertical speed indicator---------------------------------44, 51
Vertical Speed Mode (VS)----------------------------------367
Vertical Speed Reference----------------------------------367
VFR code-----------------------------------------------------123
VNAV---------------------------------------------------------188
VNV---------------------------------------------- 263, 494, 508
VNV guidance
Disabling--------------------------------------------------222
Enabling---------------------------------------------------222
VNV indications---------------------------------------------- 68
VNV Target Altitude---------------------------- 52, 370–373
VNV Target Altitude Capture Mode (ALTV)-------------374

AUDIO PANEL
& CNS

EIS

Unable to display chart----------------------------- 424, 445
Updating Garmin databases----------------------- 421, 460
Updating Jeppesen databases----------------------------442

Voice alerts, TIS----------------------------------------------- 70
Voice alerts, TIS Traffic------------------------------- 343, 482
VOL annunciation-------------------------------------------126
Voltmeter------------------------------------------------------ 88
Volume level
ADF-------------------------------------------------- 114, 116
VOR
Nearest--------------------------------------------- 179–180
VOR selection------------------------------------------------105
VSI-------------------------------------------------------------265
Vspeed references---------------------------------------45, 47
VS TGT------------------------------------------------- 224, 263

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Traffic Annunciation-------------------------------------45, 70
Traffic Information Service (TIS)-------------------- 513–514
Voice alerts------------------------------------------------- 70
Transponder----------------------------------------------------- 3
Transponder code entry------------------------------------122
Transponder data box-----------------------------------91, 93
Transponder ground mode--------------------------------119
Transponder mode field----------------------- 119, 120, 121
Transponder softkeys---------------------------------------119
Transponder standby mode-------------------------------120
Transponder status box------------------------------------- 44
Trend Vector
Turn Rate--------------------------------------------------- 56
Trend Vector, Airspeed--------------------------------------- 46
Trim, Manual Electric-------------------------- 357, 359, 386
Trip Planning------------------------------------ 239, 240, 241
Trip statistics------------------------------------------ 240, 241
True Airspeed-------------------------------------- 44, 46, 241
Tuning ADF frequencies------------------------------------115
Turn anticipation--------------------------------------------511
Turn Rate Indicator--------------------------------------44, 56
TX indicator--------------------------------------------------- 97

I-5

INDEX

APPENDICES

ADDITIONAL
FEATURES
AFCS

HAZARD
AVOIDANCE

FLIGHT
MANAGEMENT

AUDIO PANEL
& CNS
EIS

FLIGHT
INSTRUMENTS

SYSTEM
OVERVIEW

Index

Blank Page

I-6

Garmin G1000 Pilot’s Guide for the Diamond DA40/40F

190-00592-06 Rev. A

Untitled-1 1

11/13/2007 9:15:37 AM

G1000

G1000 Pilot’s Guide

Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282

Integrated Flight Deck
Pilot’s Guide

Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138

Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251

www.garmin.com

Diamond
DA40/40F

Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099

190-00592-06
Revision A

System Software 0321.20 or later

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Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, 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Inches, Inches, Inches, Inches, Inches
Manifest Reference Instance ID  : uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:d9c0c6f4-bc71-11db-bab5-ae7ba2511eae, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:F328171EDDE7DD11A6CF8DBFF0F83019, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:6577EA1FDDE7DD11A6CF8DBFF0F83019, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:971C131650F9DD11BF8099BCC06FE3DE, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:e1207b28-b22b-456a-b32b-f7ea5ba16e7e, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:16d84648-f4fb-11dc-b6f7-a3109190e281, uuid:74B1498E4F19DE119631F90539D1D126, 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Garmin Diamond Da40 Users Manual

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