Garmin Software Version 0563 05 Cockpit Reference Guide 190 00384 08_0A

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Integrated Flight Deck
Cockpit Reference Guide

Cessna
Nav III

Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reﬂects the operation of System Software version 0563.05 or later for Cessna 172R, 172S, 182T, T182T, 206H, and T206H
aircraft. 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
Web Site 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.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications; and XM®
is a registered trademark of XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell
International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.

November, 2007

190-00384-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

Printed in the U.S.A.

WARNINGS,
CAUTIONS, & NOTES

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: 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: 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: 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.
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. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition
of conﬂicting trafﬁc.
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: GDL 69 Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69 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.
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

WARNINGS,
CAUTIONS, & NOTES

WARNING: The Garmin G1000, as installed in Cessna Nav III aircraft, 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: 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 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 identiﬁed as severe or giving an
intense radar echo.”
WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according
to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
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 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 ANTIREFLECTIVE 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.
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

WARNINGS,
CAUTIONS, & NOTES

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.
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 subject to change and may not reﬂect the most current G1000 system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
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: The GDU 1040 and GDU 1044B 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 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. If you have any questions or would like additional information, please refer to our web site 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 yards
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 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

RECORD OF REVISIONS

Part Number
190-00384-03
(Rev. A)

190-00384-03
(Rev. B)
190-00384-04
(Rev. A)

Reformatted manual to new format
Added TAS capability

190-00384-04
(Rev. B)

Added DONE Softkey, XM-INFORMATION Page, and XM-RADIO
Page operation.

190-00384-05
(Rev. A)

Added explanation of EIS display behavior upon exceedances
Added better explanation of Intercom System Isolation
Added Stormscope operation upon loss of heading input
Added TAWS-B
Added CO Guardian
Added new Fuel Totalizer
Updated G1000 System Messages
Added GDU 7.00 (WAAS, VNAV & Charts) software parameters.
Added AFCS for the 182 and 206
Added database loading instructions
Updated G1000 System Messages
Combined previous system software numbers into 0563.00
Added GDU 8.02 parameters, Airways, and ADS-B

190-00384-06
(Rev A)

190-00384-07
190-00384-08

190-00384-08 Rev. A

Change Summary
Added XM Radio and XM Weather
Added ADF capability
Added DME capability
Added BRG1/BRG2 pointers
Added dual audio panel operation
Added C172 parameters
Changed Airspeed Trend Vector
Changed Altitude Trend Vector
Added Checklist capability
Added Flight ID capability
Updated system software numbers

Added GDU 8.20 parameters, including gradient background on
the PFD and GFC 700 for the C172.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

RR-1

RECORD OF REVISIONS

Revision Date of Revision Affected Pages
A
November, 2007
i through Index-4

RR-2

Description
Production release

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

TABLE OF CONTENTS
SECTION 1: SYSTEM OVERVIEW.................................... 1-1
1.1
1.2
1.3
1.4
1.5
1.6
1.7
1.8

PFD/MFD Controls................................................... 1-2
PFD Softkeys............................................................ 1-5
MFD Softkeys .......................................................... 1-8
MFD Page Groups ................................................... 1-9
Vertical Navigation .............................................. 1-10
Backlighting ........................................................... 1-12
XM Radio - Automatic Muting ........................... 1-12
Database Updates ................................................ 1-12
Jeppesen Aviation Database ...................................... 1-12
Garmin Databases..................................................... 1-13

SECTION 2: FLIGHT INSTRUMENTS .............................. 2-1
2.1 Airspeed Indicator.................................................. 2-3
Speed Indication ......................................................... 2-3
Speed Ranges ............................................................. 2-3
Airspeed Trend Vector ................................................. 2-3
Vspeed References ...................................................... 2-3
2.2 Attitude Indicator .................................................. 2-3
2.3 Altimeter .................................................................. 2-4
Selected Altitude Bug .................................................. 2-4
Altitude Trend Vector ................................................... 2-4
Barometric Setting Box ................................................ 2-4
Altitude Alerting .......................................................... 2-4
Metric Display ............................................................. 2-5
Low Altitude Annunciation........................................... 2-5
2.4 Vertical Deviation/Glidepath/Glideslope
Indicator ................................................................... 2-6
2.5 Marker Beacon Annunciations ............................ 2-7
2.6 Vertical Speed Indicator ....................................... 2-7
2.7 Barometric Altitude Minimums ........................... 2-7
2.8 Horizontal Situation Indicator (HSI) ................... 2-8
Course Pointer ............................................................ 2-9
Course Deviation Indicator (CDI) .................................. 2-9
Bearing Pointers and Information Windows ................ 2-11
DME (optional).......................................................... 2-11
Navigation Source ..................................................... 2-11
2.9 Wind Data............................................................... 2-12
2.10 Generic Timer ........................................................ 2-13

SECTION 3: ENGINE INDICATION SYSTEM (EIS).... 3-1
3.1 Engine Display......................................................... 3-1

190-00384-08 Rev. A

3.2 Lean Display ............................................................ 3-4
Normally-aspirated Aircraft .......................................... 3-7
Turbocharged Aircraft .................................................. 3-7
3.3 System Display........................................................ 3-7

SECTION 4: NAV/COM AND TRANSPONDER .......... 4-1
4.1
4.2
4.3
4.4
4.5

Radio Status Indications ....................................... 4-3
Volume ...................................................................... 4-3
Automatic Squelch ................................................. 4-3
Quickly Activating 121.500 MHz .......................... 4-3
Optional NAV Radios ............................................. 4-3
DME Radio (optional) .................................................. 4-3
ADF Radio (optional) ................................................... 4-4
4.6 Frequency Auto-tuning ......................................... 4-4
Auto-tuning on the PFD .............................................. 4-4
Auto-tuning on the MFD ............................................. 4-4
4.7 Transponder ............................................................. 4-4
Mode Selection ........................................................... 4-4
Reply Status ................................................................ 4-5
Code Selection ............................................................ 4-5
Flight ID Reporting ...................................................... 4-6

SECTION 5: AUDIO PANEL ................................................ 5-1
5.1 COM Radio Selection ............................................. 5-2
5.2 Cabin Speaker ......................................................... 5-2
5.3 Passenger Address (PA) System (T)182T and
(T)206H Only ............................................................ 5-2
5.4 Marker Beacon Receiver ....................................... 5-2
Marker Beacon Signal Sensitivity ................................. 5-2
5.5 Nav Radio Audio Selection ................................... 5-3
5.6 Intercom System (ICS) Isolation .......................... 5-3
5.7 Intercom Squelch Control ..................................... 5-4
5.8 Digital Clearance Recorder and Player ............. 5-4

SECTION 6: AUTOMATIC FLIGHT CONTROL ............. 6-1
6.1 AFCS Controls .......................................................... 6-1
6.2 Flight Director Operation ..................................... 6-2
Activating the Flight Director ....................................... 6-2
Command Bars ........................................................... 6-2
AFCS Status Box ......................................................... 6-3
6.3 Flight Director Modes............................................ 6-3
Pitch Modes ................................................................ 6-3
Roll Modes................................................................ 6-17

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

TABLE OF CONTENTS
6.4 Autopilot Operation ............................................ 6-22
Flight Control ............................................................ 6-22
Engaging the Autopilot.............................................. 6-22
Control Wheel Steering.............................................. 6-23
Disengaging the Autopilot ......................................... 6-23
6.5 Example Procedures ............................................ 6-24
Departure ................................................................. 6-25
Intercepting a VOR Radial .......................................... 6-26
Flying a Flight Plan/GPS Course ................................. 6-27
Descent .................................................................... 6-28
Approach .................................................................. 6-31
Go Around/Missed Approach ..................................... 6-33
6.6 AFCS Annunciations and Alerts ......................... 6-34
AFCS Status Alerts..................................................... 6-34
Overspeed Protection ................................................ 6-35

SECTION 7: NAVIGATION .................................................. 7-1
7.1 Navigation Map Page ............................................ 7-1
7.2 Direct-to Navigation .............................................. 7-1
Direct-to Navigation from the MFD .............................. 7-1
Direct-to Navigation from the PFD ............................... 7-3
7.3 Navigating an Example Flight Plan .................... 7-5
7.4 Airport Information ............................................. 7-21
7.5 Intersection Information .................................... 7-23
7.6 NDB Information................................................... 7-24
7.7 VOR Information ................................................... 7-24
7.8 User Waypoint Information Page ..................... 7-25
7.9 Nearest Airports ................................................... 7-25
Nearest Airport Information on the MFD .................... 7-25
Nearest Airports Information on the PFD .................... 7-26
7.10 Nearest Intersections .......................................... 7-26
7.11 Nearest NDB .......................................................... 7-27
7.12 Nearest VOR ........................................................... 7-27
7.13 Nearest User Waypoint........................................ 7-28
7.14 Nearest Frequencies ............................................ 7-28
7.15 Nearest Airspaces ................................................. 7-29

SECTION 8: FLIGHT PLANNING ...................................... 8-1
8.1 User Deﬁned Waypoints........................................ 8-1
Select the User WPT Information Page ......................... 8-1
Create User Waypoints from the Navigation Map Page. 8-2
8.2 Viewing the Active Flight Plan ............................ 8-2
8.3 Activate a Stored Flight Plan............................... 8-2

8.4
8.5
8.6
8.7
8.8
8.9
8.10
8.11
8.12
8.13
8.14
8.15
8.16
8.17
8.18
8.19
8.20

Activate a Flight Plan Leg .................................... 8-3
Stop Navigating a Flight Plan.............................. 8-3
Invert Active Flight Plan ....................................... 8-3
Create a New Flight Plan ...................................... 8-4
Create a New Flight Plan Using the MFD ..................... 8-4
Create a New Flight Plan Using the PFD ...................... 8-4
Enter an Airway in a Flight Plan ......................... 8-5
Load a Departure ................................................... 8-6
Load an Arrival........................................................ 8-6
Load an Approach .................................................. 8-6
Remove a Departure, Arrival, Approach, or
Airway from a Flight Plan .................................... 8-6
Store a Flight Plan .................................................. 8-6
Edit a Stored Flight Plan ....................................... 8-7
Delete a Waypoint from the Flight Plan............ 8-7
Invert and Activate a Stored Flight Plan .......... 8-7
Copy a Flight Plan .................................................. 8-7
Delete a Flight Plan ............................................... 8-8
Graphical Flight Plan Creation ............................ 8-8
Trip Planning............................................................ 8-8

SECTION 9: PROCEDURES ................................................ 9-1
9.1 Arrivals and Departures........................................ 9-1
Load and Activate a Departure Procedure .................... 9-1
Load and Activate An Arrival Procedure ........................ 9-1
9.2 Approaches .............................................................. 9-2
Load and/or Activate an Approach Procedure ............... 9-3
Activate An Approach in the Active Flight Plan ............. 9-3

SECTION 10: HAZARD AVOIDANCE ........................... 10-1
10.1 Customizing the Hazard Displays on the
Navigation Map .................................................... 10-1
10.2 STORMSCOPE® (Optional).................................. 10-1
Displaying Stormscope Lightning Data on the
Navigation Map Page ................................................ 10-1
Stormscope Page....................................................... 10-2
10.3 XM Weather (Service Optional) ......................... 10-3
Displaying METAR and TAF information on the
Airport Information Page ........................................... 10-3
Displaying Weather on the Weather Data Link Page ... 10-4
Map Panning Information – Weather Data Link Page . 10-5
Weather Products & Symbols ..................................... 10-5
Weather Product Age ................................................ 10-6

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

TABLE OF CONTENTS
10.4 Trafﬁc Systems ...................................................... 10-7
Trafﬁc Information Service (TIS) .................................. 10-7
Trafﬁc Advisory System (TAS) (Optional) ..................... 10-8
ADS-B Trafﬁc (Optional) ............................................. 10-9
10.5 Terrain and Obstacle Proximity ....................... 10-10
Displaying Terrain and Obstacles on the Terrain
Proximity Page ........................................................ 10-10
Displaying Terrain and Obstacles on the Navigation
Map........................................................................ 10-11
10.6 Terrain Awareness & Warning System
(TAWS) Display (Optional) ................................ 10-11
Displaying Terrain on the TAWS Page ....................... 10-11
Enable/Disable Aviation Data ................................... 10-12
TAWS Inhibit ........................................................... 10-12
Manual System Test................................................. 10-13
Forward Looking Terrain Avoidance (FLTA) ................ 10-13
Premature Descent Alert (PDA) ................................ 10-13
Excessive Descent Rate Alert (EDR) .......................... 10-14
Negative Climb Rate After TakeoffAlert (NCR) .......... 10-14
“Five-Hundred” Aural Alert...................................... 10-14
Displaying Terrain and Obstacles on the Navigation
Map........................................................................ 10-14
Pop-up Alerts .......................................................... 10-15
TAWS Alerts Summary ............................................. 10-16
Alert Annunciations ................................................. 10-17

12.3 CO Guardian Messages ....................................... 12-3
12.4 AFCS Alerts............................................................. 12-4
System Status Annunciation....................................... 12-4
12.5 TAWS Alerts............................................................ 12-5
12.6 Other G1000 Aural Alerts .................................... 12-6
12.7 G1000 System Annunciations ............................ 12-7
12.8 G1000 System Message Advisories .................. 12-9
MFD & PFD Message Advisories............................... 12-10
Database Message Advisories .................................. 12-11
GMA 1347 Message Advisories ............................... 12-13
GIA 63 Message Advisories ..................................... 12-13
GIA 63W Message Advisories .................................. 12-16
GEA 71 Message Advisories .................................... 12-18
GTX 33 Message Advisories..................................... 12-19
GRS 77 Message Advisories..................................... 12-19
GMU 44 Message Advisories ................................... 12-20
GDL 69A Message Advisories .................................. 12-20
GDC 74A Message Advisories.................................. 12-20
Miscellaneous Message Advisories........................... 12-21

INDEX ...................................................................................Index-1

SECTION 11: ABNORMAL OPERATION ..................... 11-1
11.1
11.2
11.3
11.4

Reversionary Mode .............................................. 11-1
Abnormal COM Operation .................................. 11-2
Unusual Attitudes ................................................. 11-2
Stormscope Operation with loss of
Heading Input........................................................ 11-2
11.5 Hazard Displays with Loss of GPS Position .... 11-2
11.6 Dead Reckoning .................................................... 11-3

SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1
12.1 Alert Level Deﬁnitions ........................................ 12-2
12.2 NAV III Aircraft Alerts .......................................... 12-3
WARNING Alerts ....................................................... 12-3
CAUTION Alerts ........................................................ 12-3
CAUTION Alerts (T182, T206, and 206 with Prop
De-Ice Only) .............................................................. 12-3
Safe Operating Annunciation (T182, T206, and 206
with Prop De-Ice Only) .............................................. 12-3

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

iii

TABLE OF CONTENTS

Blank Page

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW

SECTION 1: SYSTEM OVERVIEW
The purpose of this Cockpit Reference Guide is
to provide the pilot a resource with which to ﬁnd
operating instructions on the major features of the
G1000 system more easily. It is not intended to be a
comprehensive operating guide. Complete operating
procedures for the complete system are found in the
Garmin G1000 Pilot’s Guide for the Cessna Nav III (19000498-03).

190-00384-08 Rev. A

This guide gives the pilot abbreviated operating
instructions for the Primary Flight Display (PFD), Multi
Function Display (MFD), and the GMA 1347 Audio Panel
System.
NOTE: The pilot should read and thoroughly
understand the Cessna Pilot’s Operating
Handbook (POH) for limitations, procedures and
operational information not contained in this
Cockpit Reference Guide. The Cessna POH always
takes precedence over the information found in
this guide.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-1

SECTION 1
SYSTEM OVERVIEW

1.1

PFD/MFD CONTROLS
1

17
18

GFC 700 AFCS Only
1-2

Figure 1-1 PFD/MFD Controls
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW
PFD and MFD controls function the same.

COM Frequency Transfer Key – Transfers the
standby and active COM frequencies. Pressing
and holding this key for two seconds automatically
tunes the emergency frequency (121.5 MHz) in
the active frequency ﬁeld.

COM VOL/SQ Knob – Controls COM audio level.
Pressing this knob turns the COM automatic
squelch ON and OFF. Audio volume level is
shown in the ﬁeld as a percentage.

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

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

Dual NAV Knob – Tunes the MHz (large knob)
and kHz (small knob) standby frequencies for
the NAV receiver. Press to switch the tuning box
(light blue box) between the NAV1 and NAV2
ﬁelds.

Heading Knob – Turn to manually select a heading
on the HSI. When pressed, it synchronizes
the heading bug with the compass lubber line.
Selected Heading provides the heading reference
to the Flight Director while operating in Heading
Select Mode.

Direct-to Key – Allows the user to enter a
destination waypoint and establish a direct course
to the selected destination (speciﬁed by the
identiﬁer, chosen from the active route, or taken
from the map pointer position).

FPL Key – Displays the active Flight Plan Page for
creating and editing the active ﬂight plan, or for
accessing stored ﬂight plans.

CLR Key (DFLT MAP) – Erases information,
cancels an entry, or removes page menus. To
display the Navigation Map Page immediately,
press and hold CLR (MFD only).

Dual FMS Knob – Used to select the page to
be viewed (only on the MFD). The large knob
selects a page group (MAP, WPT, AUX, NRST),
while the small knob selects a speciﬁc page within
the page group. Pressing the small knob turns the
selection cursor ON and OFF. When the cursor
is ON, data may be entered in the different ﬁelds
using the small and large knobs. The large knob
is used to move the cursor on the page, while the
small knob is used to select individual characters
for the highlighted cursor location. When the
G1000 displays a list that is too long for the
display screen, a scroll bar appears along the right

Joystick – Changes the map range (distance top to
bottom of map display) when rotated. Activates
the map pointer when pressed.

CRS/BARO Knob – The large knob sets the
altimeter barometric pressure and the small knob
adjusts the course. The course is only adjustable
when the HSI is in VOR1, VOR2, or OBS/SUSP
Mode. Pressing this knob centers the CDI on the
currently selected VOR. Selected Course provides
course reference to the Flight Director when
operating in Navigation and Approach Modes.

Dual COM Knob – Tunes the MHz (large knob)
and kHz (small knob) standby frequencies for the
COM transceiver. Pressing this knob switches the
tuning box (light blue box) between the COM1
and COM2 ﬁelds.

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-3

SECTION 1
SYSTEM OVERVIEW
side of the display, indicating the availability of
additional items within the selected category.
Press the small FMS Knob to activate the cursor
and turn the large FMS Knob to scroll through the
list.
14

MENU Key – Displays a context-sensitive list
of options. This list allows the user to access
additional features, or to make setting changes
that relate to certain pages.
PROC Key – Selects approaches, departures and
arrivals from the ﬂight plan. If a ﬂight plan is
used, available procedures for the departure and/
or arrival airport are automatically suggested. If
a ﬂight plan is not used, the desired airport and
the desired procedure may be selected. This key
selects IFR departure procedures (DPs), arrival
procedures (STARs) and approaches (IAPs) from
the database and loads them into the active ﬂight
plan.
ENT Key – Accepts a menu selection or data
entry. This key is used to approve an operation
or complete data entry. It is also used to conﬁrm
selections and information entries.

Flight Director and engages the Autopilot in the
default pitch axis and roll axis modes. Pressing
the AP Key again disengages the autopilot and
deactivates the Flight Director.
19

HDG Key – Selects/deselects the Heading Select
Mode.

NAV Key – Selects/deselects the Navigation
Mode.

APR Key – Selects/deselects the Approach Mode.

VS Key – Selects/deselects the Vertical Speed
Mode.

FLC Key – Selects/deselects the Flight Level
Change Mode.

FD Key – Activates/deactivates the Flight Director
only. Pressing the FD Key turns on the Flight
Director in the default pitch axis and roll axis
modes. Pressing the FD Key again deactivates the
Flight Director and removes the command bars,
unless the Autopilot is engaged. If the Autopilot
is engaged, the FD Key is disabled.

ALT Key – Selects/deselects the Altitude Hold
Mode.

VNV Key – Selects/deselects Vertical Navigation
Mode.

BC Key – Selects/deselects Back Course Mode.

Dual ALT Knob – Sets the selected altitude in
the box located above the Altimeter. The large
knob selects the thousands, while the small knob
selects the hundreds. Altitude Select is used by
the Automatic Flight Control System in certain
modes, in addition to the standard G1000 Altitude
Alerter function.
The following are only available with the GFC 700
AFCS.
18

1-4

AP Key – Engages/disengages the Autopilot and
Flight Director. Pressing the AP Key activates the

28 29

NOSE UP/NOSE DN Keys – Controls the
active pitch reference for the Pitch Hold,
Vertical Speed, and Flight Level Change
Modes.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW

1.2

PFD SOFTKEYS
Softkey ON

Softkey OFF

Figure 1-2 PFD Top Level Softkeys
DME

ALERTS

STRMSCP

ALERTS

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

Figure 1-3 INSET Softkeys

INSET – Press to display the Inset Map in the lower
left corner of the PFD.
OFF – Press to remove the Inset Map.
DCLTR (3) – Press momentarily to select the desired
amount of map detail. The declutter level appears
adjacent to the DCLTR Softkey.
- No declutter: All map features are visible.
- Declutter – 1: Declutters land data.
- Declutter – 2: Declutters land and SUA data.
- Declutter – 3: Declutters large NAV data
remaining (removes everything except the
active ﬂight plan).
TRAFFIC – Press to display trafﬁc on the map.

190-00384-08 Rev. A

TOPO – Press to display topographical data (i.e.,
coastlines, terrain, rivers, lakes, etc.) and
elevation scale on the Inset Map.
TERRAIN – Press to display terrain information on
the Inset Map.
STRMSCP (optional) – Press to display the
Stormscope lightning data on the Inset Map
(within a 200 nm radius of the aircraft).
NEXRAD (optional) – Press to display NEXRAD
weather and coverage information on the Inset
Map.
XM LTNG (optional) – Press to display XM lightning
information on the Inset Map.
BACK – Press to return to the previous level softkey
conﬁguration.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-5

SECTION 1
SYSTEM OVERVIEW
DME

DME

ALERTS

ALT UNIT

HSI FRMT

BRG1 (NAV1)

BRG2 (NAV2)

BRG1 (GPS)

BRG2 (GPS)

BRG1 (ADF)

BRG2 (ADF)

BRG1 (OFF)

BRG2 (OFF)
360 HSI

ALERTS

Press the STD BARO or
BACK Softkey to return to
the top-level softkeys

ARC HSI

ALERTS

METERS

HPA

ALERTS

Figure 1-4 PFD Conﬁguration Softkeys

PFD – Press to display the additional softkeys for
additional conﬁguration of the PFD.
DFLTS – Press to reset default settings on the PFD.
WIND – Displays softkeys to select wind data
parameters.
OPTN 1 – Wind direction arrows with headwind
and crosswind components.
OPTN 2 – Wind direction arrow and speed.
OPTN 3 – Wind direction arrow with direction
and speed.
OFF – Information not displayed.
DME (optional) – Press to display the DME
Information Window.
BRG1 (bearing) – Press to cycle through the
following Nav sources, making the pointer the
indicator for the corresponding source and
displaying the appropriate information.
NAV1 – Displays NAV1 waypoint frequency or
identiﬁer and DME information in the BRG1
Information Window.
1-6

GPS – Displays GPS waypoint identiﬁer and GPS
distance information in the BRG1 Information
Window.
ADF – Displays ADF in the BRG1 Information
Window when an otional ADF is installed.
OFF – Removes the BRG1 Information
Window.
HSI FRMT – Press to display the HSI formatting
softkeys.
360 HSI – Press to display the HSI in a 360
degree format.
ARC HSI – Press to display the HSI in an arc
format.
BRG2 (bearing) – Press to cycle through the
following Nav sources, making the pointer the
indicator for the corresponding source and
displaying the appropriate information.
NAV2 – Displays NAV2 waypoint frequency or
identiﬁer and DME information in the BRG2
Information Window.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW
GPS – Displays GPS waypoint identiﬁer and GPS
distance information in the BRG2 Information
Window.
ADF – Displays ADF in the BRG2 Information
Window when an otional ADF is installed.
OFF – Removes the BRG2 Information
Window.
ALT UNIT – Displays softkeys for setting the
altimeter and BARO settings to metric units:
METERS – When enabled, displays altimeter in
meters.
IN – Press to display the BARO setting as inches
of mercury.
HPA – Press to display the BARO setting as
hectopacals.
STD BARO – Press to set the barometric pressure
to standard pressure.
BACK – Press to return to the previous level softkeys.
ALERTS – Press to display the Alerts Window.
OBS – Press to select OBS Mode on the CDI when
navigating by GPS (only available with active leg).
CDI – Press to change navigation mode on the CDI
between GPS, VOR1, and VOR2.
DME (optional) – Press to display the DME Tuning
Window.

XPDR – Press to display the transponder mode
selection softkeys.
STBY – Press to select Standby Mode.
ON – Press to select Mode A.
ALT – Press to select Altitude Reporting Mode.
GND – Press to select Ground Mode.
VFR – Press to automatically squawk 1200 (only
in the U.S.A., refer to ICAO standards for VFR
codes in other countries).
CODE – Press to display transponder code selection
softkeys 0-7.
0 through 7 – Press numbers to enter code.

IDENT – Press to provide special aircraft
position identiﬁcation to Air Trafﬁc Control
(ATC).
BKSP – Press to remove numbers entered one
at a time.
BACK – Press to return to the previous level
softkeys.
IDENT – Press to provide special aircraft position
identiﬁcation to Air Trafﬁc Control (ATC).
BACK – Press to return to the previous level
softkeys.
ALERTS – Press to display the Alerts Window.
DME

ALERTS

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

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

Figure 1-5 XPDR (Transponder) Softkeys
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-7

SECTION 1
SYSTEM OVERVIEW
IDENT – Press to provide special aircraft position
identiﬁcation to Air Trafﬁc Control (ATC).
TMR/REF – Press to display the Timer/References
Window.
NRST – Press to display the Nearest Airports
Window.
ALERTS – Press to display the Alerts Window.

1.3

MFD SOFTKEYS

MAP – Pressing this softkey enables the following
softkeys:
TRAFFIC – Pressing this softkey displays/removes
Trafﬁc on the Navigation Map.
TOPO – Pressing this softkey displays or removes
topographic information on the Navigation Map.
TERRAIN – Pressing this softkey displays/removes
terrain and obstacle data on the Navigation Map.

ENGINE – Pressing this softkey makes available the LEAN
and SYSTEM Softkeys which in turn access the Lean
Page and the System Page, respectively.
ENGINE

DCLTR

MAP

SHW CHRT

CHKLIST

(optional)

DCLTR-1

LEAN

ENGINE

SYSTEM

BACK

DCLTR-2
DCLTR-3

ENGINE

LEAN

SYSTEM

RST FUEL

GAL REM

(Default softkey
is dependant on
the selection made
in the map setup
options)

BACK
TRAFFIC

TOPO

TERRAIN

AIRWAYS

Press the BACK Softkey on this
level to return to the top softkey level.
(optional)

(optional)

STRMSCP

NEXRAD

XM LTNG

BACK

AIRWY ON

AIRWY LO
AIRWAY HI

Press the BACK Softkey to return
to the previous softkey level.

Press the ENGINE Softkey to
the default Engine Page level.
ENGINE

LEAN

SYSTEM

-10 GAL

-1 GAL

+1 GAL

+10 GAL

XX GAL

BACK

X = airframe specific values

Press the ENGINE or BACK Softkey to
return to the default Engine Page level.
ENGINE

LEAN

SYSTEM

CYL SLCT

ASSIST

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

ENGINE

DONE

EXIT

EMERGCY

Figure 1-6 MFD Softkeys
1-8

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW
AIRWAYS – Pressing this softkey displays/removes
airways information. The default is dependent on
map setup option selected. Pressing cycles through
all airways displayed (AIRWY ON), low altitude
airways only (AIRWY LO), and high altitude airways
only (AIRWY HI).
STRMSCP (optional) – Pressing this softkey displays/
removes Stormscope lightning data on the Navigation
Map.
NEXRAD (optional) – Pressing this softkey displays/
removes precipitation data on the Navigation Map.
XM LTNG (optional) – Pressing this softkey displays/
removes XM Radio lightning data on the Navigation
Map.
BACK – Pressing this softkey displays the ENGINE and
MAP top level softkeys.
DCLTR (declutter) – Pressing this softkey removes map
information in three levels.
SHW CHRT (Show Chart)(optional) – Pressing this softkey
displays optional FliteCharts or ChartView charts.
CHKLIST (checklist)(optional) – Pressing the CHKLIST
Softkey displays the Checklist Page.
ENGINE – Displays engine softkeys.
DONE – Pressing this softkey checks off a checklist item.
If an item is already checked, an UNDO Softkey is
displayed.
EXIT – Press to exit the checklist.
EMERGCY – Pressing this softkey displays the
emergency checklist.

1.4

MFD PAGE GROUPS

1) Turn the large FMS Knob until the desired page
group is selected.
2) Turn the small FMS Knob to select pages within the
group. See Figure 1-7.

Nearest Group
Auxiliary Page Group

Number of Pages in Current
Group

Waypoint Page Group
Map Page Group
Figure 1-7 Page Group Icon
190-00384-08 Rev. A

Selected Page

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-9

SECTION 1
SYSTEM OVERVIEW

1.5

VERTICAL NAVIGATION

One of two altitude sources is used by the G1000 when
giving vertical navigation guidance. WAAS GPS altitude
is used when giving guidance for a WAAS approach after
the Final Approach Fix. Baro corrected altitude is used
when vertical guidance is given in all other situations and
in non-WAAS systems.
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, entered by the pilot 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.
NOTE: All arrival procedure altitudes contained in
the navigation database are for turbojet aircraft only.
Alter or enter altitudes as desired to comply with the
ATC clearance.

When activating or loading an arrival or approach
procedure into an active ﬂight plan, the VNV ‘ALT’ ﬁelds
are populated with any altitudes that can be retrieved
from the navigation database.
Since altitudes loaded with an arrival procedure are
published only for turbojet aircraft, the altitudes are
displayed as white text indicating that the altitudes are
displayed for reference only. An arrival waypoint altitude
may be used (or “designated”) as is, or changed to a
different altitude. An altitude is designated by pressing the
FMS Knob and turning the large FMS Knob to place the
cursor on the desired altitude and pressing the ENT Key or
entering a different value and pressing the ENT Key. The
altitude is now displayed as light blue text, indicating that
1-10

the altitude is now designated to give vertical speed and
deviation guidance.
Approach waypoint altitude constraints are automatically
designated when the approach is loaded. These altitudes
are also displayed as light blue text. Waypoint altitude
constraints designated 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 manually.
Altitudes that have been designated for use in vertical
guidance may also be made “non-designated” by placing the
cursor over the desired altitude and pressing the CLR Key.
Other displayed altitudes may change due to re-calculations
or rendered invalid as a result of manually changing an
altitude to a non-designated altitude.
To help interpret the meanings of how the altitudes are
presented, keep the following points in mind:
• When the altitude is displayed in light blue,
the system is using that altitude (designated) to
determine vertical speed and deviation guidance.
• When the altitude is displayed in white, it is not being
used by the system (non-designated) to determine
the vertical speed and deviation guidance.
• An altitude displayed as small text is an altitude that
is published in the navigation database.
• Altitudes displayed as a light blue subdued text
cannot be used in the current vertical navigation
calculations.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW
White Text

Light Blue Text

Light Blue Subdued Text

Large Text

Altitude calculated by the system
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 has been entered by the
pilot. 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.

The system cannot use this altitude
in determining vertical speed and
deviation guidance.

Small Text

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.

Altitude is designated for use in
giving vertical speed and deviation
guidance. Altitude has been
retrieved from the navigation
database or has been entered by
the pilot and matches a published
altitude in the navigation database.

The system cannot use this altitude
in determining vertical speed and
deviation guidance.

Table 1-1 VNV Altitude Text Size and Color

Refer to Figure 1-8 and Table 1-1 for more detail
regarding the signiﬁcance of text size and color.

Some altitudes retrieved from the database have
associated restrictions indicating to stay ‘At’, ‘At or Above’,
or ‘At or Below’ a speciﬁc altitude. These restrictions are
indicated using a ‘bar’ above and/or below the appropriate
Large White altitude as shown in Figure 1-9.
Text

Large Light
Blue Text

Cross AT or ABOVE 5,000 ft

Small Light
Blue Text

Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft

Small Light
Blue Subdued
Text

Figure 1-8 VNAV Altitudes

190-00384-08 Rev. A

Figure 1-9 Altitude Restrictions

Small White
Text with
Altitude
See Section 7 - Navigation, for a sample ﬂight plan
Restriction
which further illustrates vertical navigation in more
Bar

detail.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-11

SECTION 1
SYSTEM OVERVIEW

1.6

BACKLIGHTING

1.8

Manually adjust the backlight for the PFD
and MFD:
1) Press the MENU Key on the PFD to display the PFD
Setup Menu window.
2) Press the small FMS Knob to activate the cursor.
‘PFD DSPL > AUTO’ is now highlighted.
3) Turn the small FMS Knob to display the
selection window.
4) Turn the small FMS Knob to select ‘MANUAL’, then
press the ENT Key.
5) With the intensity value now highlighted, turn
the small FMS Knob to select the desired
backlighting.
6) Turn the large FMS Knob to highlight ‘MFD DSPL
> AUTO’ and repeat steps 3 through 5.

DATABASE UPDATES

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.
The following procedures pertain to updating the
G1000 system with SD cards as outlined in Appendix B of
the G1000 Cessna Nav III Pilot’s Guide.

Jeppesen Aviation Database
NOTE: After the aviation database is installed,
the card may be removed after loading the
update to each LRU.

Updating the Jeppesen aviation database:
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 facing left).
2) Turn the G1000 System ON. A prompt similar to
the following is displayed in the upper left corner
of the PFD:

Figure 1-10 PFD Setup Menu Window

1.7

XM RADIO - AUTOMATIC MUTING

XM Radio audio is automatically muted when the
aircraft groundspeed exceeds approximately 30 kts and
the airspeed is less than approximately 80 kts. The audio
must be manually unmuted once the aircraft is outside
the applicable speed range. Refer to the G1000 Optional
Equipment section of the pilot’s guide.
1-12

Figure 1-11 Database Update Prompt

3) Press the ENT Key to start the database update. A
prompt similar to the following is displayed:

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 1
SYSTEM OVERVIEW
2) Apply power to the G1000 System. View the MFD
power-up splash screen. Check that the databases
are initialized and displayed on the scrolling
window of 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.
Figure 1-12 Database Update Conﬁrmation

4) After the update completes, the PFD starts in normal
mode.
5) Turn the G1000 System OFF and remove the SD
card.
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 that the correct update cycle is loaded during
startup of the MFD.

Garmin Databases
Since these databases are not stored internally in the
MFD or PFD, a Supplemental Data Card containing identical database versions must be kept in each display unit.
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.

1) Insert one SD card in the bottom card slot of the
MFD and one in the bottom card slot of the PFD.
The SD card containing the ChartView or FliteCharts
database must be inserted into the bottom slot on
the MFD.
190-00384-08 Rev. A

Figure 1-13 Power-Up Splash Screen Window

3) Acknowledge the Power-up Page agreement by
pressing the ENT Key or the right most softkey.
4) At the MAP – NAVIGATION MAP Page, press the
MAP Softkey and check to make sure that the TOPO
and TERRAIN Softkeys are available (not dimmed)
and other database features are functioning.
5) Power down the G1000.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

1-13

SECTION 1
SYSTEM OVERVIEW

Blank Page

1-14

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

SECTION 2: FLIGHT INSTRUMENTS
The following discussions pertain to the Primary Flight
Display, unless otherwise indicated.
1

14
2

13
12

6
8

7
1

NAV Frequency Box

Turn Rate Indicator

Airspeed Indicator

Barometric Setting Box

True Airspeed Box

Vertical Speed Indicator

Heading Box

Altimeter

Ground Track Bug

Selected Altitude Box

Horizontal Situation Indicator

COM Frequency Box

Outside Air Temperature Box

Navigation Status Box

System Time Box

Slip/Skid Indicator

Transponder Status Box

Attitude Indicator

Figure 2-1 Default PFD Information
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-1

SECTION 2
FLIGHT INSTRUMENTS

13
12

3
11
4

6
1

Trafﬁc Annunciation

Vspeed References

Selected Heading Box

Wind Data Window

Inset Map

BRG1 Information Window

DME Information Window

BRG2 Information Window

Flight Plan Window

Barometric Minimums Box

Selected Altitude Bug

Selected Course Box

Barometric Minimums Bug

Vertical Deviation/Glidepath (WAAS enabled systems only)/Glidesope Indicator
15 Marker Beacon Annunciation

Figure 2-2 Additional PFD Information
Active Flight Plan Leg

Distance to Next
Waypoint

Bearing to Next
Waypoint

Figure 2-3 PFD Navigation Status Box
2-2

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

2.1

AIRSPEED INDICATOR

Actual Airspeed

Vspeed References

Vspeed
References

Speed Ranges
Airspeed Trend
Vector
True Airspeed
Box
Figure 2-4 Airspeed Indicator

Vspeed References are turned on or off in the
Timer/References Window. Press the TMR/REF Softkey
to display the widow. When active (ON), the Vspeeds are
displayed at their respective locations to the right of the
airspeed scale. To activate the Vspeed References, display
the Timer/Reference Window and turn the large FMS
Knob to place the cursor in the ON/OFF ﬁeld. Turn the
small FMS Knob to select ON or OFF.

2.2

ATTITUDE INDICATOR
10

Speed Indication
The indicated airspeed is displayed inside the black
pointer. The pointer becomes red upon reaching Vne.

Figure 2-5 Red Pointer at Vne

Speed Ranges
The color coded speed range strip denotes ﬂaps
operating range, normal operating range, and never
exceed speed (Vne). A red range is also present for low
speed awareness. Refer to the Pilot’s Operating Handbook
(POH) for airspeed limitations and indicator markings.

Airspeed Trend Vector
The end of the trend vector displays approximately
what the airspeed will be in 6 seconds if the current rate
of acceleration/deceleration is maintained.

190-00384-08 Rev. A

4
5

Roll Pointer

Aircraft Wing Tips

Roll Scale

Pitch Scale

Horizon Line

Slip/Skid Indicator

Aircraft Symbol

Sky Representation

Land Representation

Roll Index Zero

Figure 2-6 Attitude Indicator

The Slip/Skid Indicator is located under the roll pointer
and moves laterally away from the pointer to indicate
lateral acceleration. One Slip/Skid indicator displacement
is equal to one ball displacement when compared to a
traditional slip/skid indicator.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-3

SECTION 2
FLIGHT INSTRUMENTS

2.3

ALTIMETER

Altitude Trend Vector
Altitude
Reference
Box

Altitude
Reference
Bug

The end of the trend vector displays approximately
what the altitude will be in six seconds if the current rate
of vertical speed is maintained.

Barometric Setting Box
Altitude
Trend
Vector

Current
Altitude

Select barometric pressure:
Turn the BARO Knob to select the desired
setting.
Quickly enter standard pressure:
1) Press the PFD Softkey.

Barometric
Altitude
Minimums Bug

2) Press the STD BARO Softkey.
Barometric
Setting
Box

Altitude Alerting
Within 1000 ft

Within 200 ft

Deviation of ±200 ft

Figure 2-7 Altimeter

Selected Altitude Bug
The Selected Altitude Bug is displayed at the Selected
Altitude or the edge of the tape (whichever is closer to the
current altitude) to provide increased altitude awareness
and to set the desired hold altitude for the autopilot.
Set the Selected Altitude Bug:

Figure 2-8 Altitude Alerting Visual Annunciations

Visual annunciations appear in the Altitude Reference
Box. Whenever the setting is changed, the Altitude
Alerter is reset. The Altitude Alerter is independent of the
Automatic Flight Control System.

Turn the ALT Knobs to set the Selected Altitude Bug.
The small ALT Knob sets the hundreds and the large
ALT Knob sets the thousands. This altitude also
appears in the Selected Altitude Box above the
Altimeter.

2-4

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

Low Altitude Annunciation

Metric Display
Display altitude in meters and barometric
pressure in hectopascals:
1) Press the PFD Softkey to display the second level
softkeys.
2) Press the ALT UNIT Softkey.
3) Press the METERS Softkey to display altitude in
meters.
4) Press the HPA Softkey to display the barometric
setting in hectopascals. Press the IN Softkey
to display the barometric setting in inches of
mercury.
5) Press the BACK Softkey to return to the previous
level softkeys.

NOTE: The LOW ALT annunciation is only available
in G1000 systems conﬁgured with WAAS-capable
GPS. Also, the LOW ALT annunciation is not
available when the G1000 is conﬁgured with
TAWS (Terrain Awareness & Warning System),
unless TAWS is inhibited.

When the Final Approach Fix (FAF) is the active
waypoint in a GPS WAAS approach using vertical guidance,
a LOW ALT (Low Altitude) annunciation may appear if
the current aircraft altitude is at least 164 feet below the
prescribed altitude at the FAF. The annunciation initially
ﬂashes. After a few seconds the ﬂashing stops and the
annunciation is displayed as shown in Figure 2-10.
Low Altitude
Annunciation

Figure 2-9 Altimeter (Metric)

190-00384-08 Rev. A

Figure 2-10 Low Altitude on GPS Approach

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-5

SECTION 2
FLIGHT INSTRUMENTS

2.4

VERTICAL DEVIATION/GLIDEPATH/
GLIDESLOPE INDICATOR

The Vertical Deviation and Required Vertical Speed
Indicators appear when vertical guidance is being given
prior to executing an approach (see Figure 2-11). In
systems that are WAAS enabled, the Glidepath Indicator
appears at a point prior to the FAF when executing an LPV,
LNAV/VNAV, or LNAV+V approach (see Figure 2-12).
VNAV
Target
Altitude

Vertical
Deviation
Indicator

Glidepath
Indicator

Figure 2-12 Glidepath Indicator
Required
Vertical
Speed

The Glideslope Indicator appears when an ILS approach
has been activated and an ILS is tuned in the active NAV
receiver ﬁeld (see Figure 2-13).
Marker Beacon
Annunciation

Figure 2-11 Vertical Deviation Indications
Glideslope
Indicator

Figure 2-13 Glideslope Indicator

2-6

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

2.5

MARKER BEACON ANNUNCIATIONS

Outer Marker

Middle Marker

Inner Marker

2.7

BAROMETRIC ALTITUDE MINIMUMS

The desired barometric altitude minimums can be set in
the Timer/References Window. The altitude ranges from 0
to 16,000 feet in 10-foot increments. The minimums are
reset anytime the power is cycled.

Figure 2-16 Barometric Minimum Descent Altitude Settings
Altimeter

Figure 2-14 Marker Beacon Annunciations

2.6

VERTICAL SPEED INDICATOR

Selected Vertical Speed

Vertical Speed Bug
Vertical Speed Pointer

The desired barometric minimum descent altitude
(MDA, or Decision Height, DH) can be set in the Timer/
References Window.
Visual annunciations alert the pilot when approaching
the MDA:
• When the aircraft altitude descends to within 2500
feet of the MDA setting, the Barometric Minimum
Box appears with the altitude in light blue text.
The bug appears on the tape in light blue once in
range.
• When the aircraft passes through 100 feet of the
MDA, the bug and text turn white.
• Once the aircraft descends past the MDA, the bug
and text turn yellow and the aural alert, “Minimums
Minimums”, is generated.
Alerting is inhibited while the aircraft is on the ground.
If the aircraft climbs after having reached the MDA, once it
reaches 50 feet above the MDA, alerting is disabled.

Figure 2-15 Vertical Speed Indicator

The actual vertical speed is displayed inside the
pointer.
When the Flight Director is placed in Vertical Speed
Mode (by pressing the VS Key) the Vertical Speed Bug
is displayed. Press the NOSE UP or NOSE DN Key to
adjust.
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-7

SECTION 2
FLIGHT INSTRUMENTS
Within 2500 ft

Within 100 ft

HSI FRMT Softkey, followed by the 360 HSI or the ARC
HSI Softkey.
15

Barometric
Minimum Bug

Barometric
Minimum Box
Altitude Reached

10
9

Figure 2-17 Barometric Minimum Descent Altitude
Alerting Visual Annunciations

Set the barometric altitude minimums:

1) Press the TMR/REF Softkey.

2) Turn the large FMS Knob to highlight the
‘Minimums’ ﬁeld (Figure 2-16).

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.

2.8

HORIZONTAL SITUATION INDICATOR
(HSI)

The HSI compass can be displayed as a 360° rose or
140° arc by pressing the PFD Softkey, followed by the
2-8

6
8
9
10
11
12
13
14
15

Turn Rate Indicator
Ground Track Bug
Lateral Deviation Scale
Navigation Source
Aircraft Symbol
Course Deviation Indicator
Rotating Compass Rose
OBS Mode
TO/FROM Indicator
Heading Bug
Course Pointer
Flight Phase
Turn Rate and Heading Trend Vector
Heading
Lubber Line

Figure 2-18 Horizontal Situation Indicator

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

Turn Rate Indicator and Heading Trend Vector
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 six
seconds, based on the present turn rate. 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.
Half-Standard Turn
Rate Tick Mark
Standard Turn
Rate Tick Mark

Turn Rate
Trend Vector
(rate > 4
deg/sec)

Figure 2-19 Turn Rate Indicator and Trend Vector
Turn Rate
Trend Vector
(standard rate)

Course Deviation Indicator (CDI)
The CDI scale automatically adjusts to the current
phase of ﬂight as seen in Figure 2-22. Scaling may be
selected manually from the MFD System Setup Page.
Flight Phase
Departure (DRPT)
Terminal (TERM)
Enroute (ENR)
Oceanic (OCN)
Approach (LNAV)
Approach (LNAV+V)
(WAAS systems only)
Approach (LNAV/
VNAV)(WAAS only)
Approach
(LPV)(WAAS only)
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 2-23)
1.0 nm decreasing to a speciﬁed
course width, then 0.3 nm,
depending on variables (see
Figure 2-24)
0.3 nm

Figure 2-20 Standard-Rate Turn Indication

Course Pointer
The course pointer is a single line arrow (GPS, VOR1
and LOC1) or double line arrow (VOR2 and LOC2) which
points in the direction of the set course.

Figure 2-21 Course Pointer
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-9

Departure

Enroute

Terminal

(Oceanic if >200 nm
from nearest airport)

0.3 nm

1.0 nm

2.0 nm

1.0 nm

0.3 nm

CDI Full-scale Deflection

SECTION 2
FLIGHT INSTRUMENTS

Refer to accompanying
approach CDI scaling figures

Missed
Approach

Approach

Drawing not to scale

2 nmFAF

CDI scale varies if Vectors-To-Final is activated

CDI scale varies if Vectors-To-Final is activated
Drawing not to scale

Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling

2-10

0.3 nm

angle based
on database
information

course width

1.0 nm

CDI Full-scale Deflection

0.3 nm

angle set
by system

350 ft

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

CDI Full-scale Deflection

Figure 2-22 Phases of Flight/CDI Scaling

Landing
Threshold

Drawing not to scale

Figure 2-24 Typical LNAV/VNAV and LPV Approach CDI Scaling
(WAAS Systems Only)

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

Bearing Pointers and Information Windows
Pressing the PFD Softkey provides access to the BRG1
and BRG2 Softkeys. The BRG1 pointer is a single line
pointer. The BRG2 pointer is a double line pointer. Press
the BRG1 or BRG2 Softkey to cycle through selecting
NAV1/2, GPS, or ADF for display using the corresponding
pointer.
DME
Information Bearing 1
Pointer
Window

Bearing 2
Pointer

CDI

Distance to
Bearing Source
Waypoint
Identiﬁer
Bearing
Pointer
Source
Icon
Figure 2-27 BRG2 Information Window

DME (optional)
To display the DME Information Window, press the
PFD Softkey followed by the DME Softkey.

Figure 2-28 DME Information Window

Navigation Source
Bearing 1
Information
Window

Bearing 2
Information
Window
Figure 2-25 HSI with Bearing Information
Distance to
Bearing Source

1) Press the CDI Softkey to change from GPS to
VOR1/LOC1.
2) Press the CDI Softkey again to change from VOR1/
LOC1 to VOR2/LOC2.
3) Press the CDI Softkey a third time to return to
GPS.

Waypoint
Identiﬁer

When using GPS as the navigation source, the following
may appear:

Bearing
Pointer
Source
Icon
Figure 2-26 BRG1 Information Window

190-00384-08 Rev. A

Change CDI navigation sources:

• LOI - GPS position integrity is inadequate for the
current procedure being ﬂown. If GPS is being
used as primary navigation, and LOI is annunciated,
other means of primary navigation is required, such
as VHF. LOI is also displayed during GPS position
initialization.
• WARN – GPS detects a position error.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-11

SECTION 2
FLIGHT INSTRUMENTS
• OBS – Displayed when operating in OBS Mode.
• SUSP – Displayed when in OBS Mode indicating
GPS waypoint sequencing is suspended.
• DR – Navigating using Dead Reckoning due to an
error in the GPS solution.

2.9

WIND DATA

When the window is selected for display, but wind
information is invalid or unavailable, the window shows
“NO WIND DATA”. Wind data can be displayed in three
different ways:
• Wind direction arrows with headwind and crosswind
components (Option 1)
• Wind direction arrow and speed (Option 2)
• Wind direction arrow with direction and speed
(Option 3)
Option 1

Option 2

Option 3

No Data

Figure 2-30 Wind Data Window

Displaying wind data:
Figure 2-29 GPS LOI, GPS SUSP, LOC1 and VOR2

Enable/disable OBS Mode while navigating
with GPS:

1) Press the PFD Softkey.
2) Press the WIND Softkey to display wind data below
the Selected Heading.

1) Press the OBS Softkey to select OBS Mode.

3) Press one of the OPTN softkeys to change how
wind data is displayed.

2) Turn the CRS Knob to select the desired course
to/from the waypoint.

4) To remove the Wind Data Window, press the OFF
Softkey.

3) Press the OBS Softkey again to disable OBS
Mode.
NOTE: The OBS Softkey is only displayed when
navigating an active leg using GPS.

2-12

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 2
FLIGHT INSTRUMENTS

2.10 GENERIC TIMER

Figure 2-31 Timer Status Prompts

Change the Generic Timer:
1) Press the TMR/REF Softkey, then turn the large FMS
Knob to select the time ﬁeld (hh/mm/ss). Turn the
FMS Knobs to set the desired time, then press the
ENT Key. The UP/DOWN ﬁeld is now highlighted.
2) Turn the small FMS Knob to display the UP/DOWN
window. Turn the FMS Knob to select ‘UP’ or
‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3) Press the ENT Key to START, STOP, or RESET the
timer (if the timer is counting DOWN, it must be
reset manually). Press the CLR Key or the TMR/REF
Softkey to remove the window.

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

2-13

SECTION 2
FLIGHT INSTRUMENTS

Blank Page

2-14

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)

SECTION 3: ENGINE INDICATION
SYSTEM (EIS)

Tachometer (RPM) – Shows propeller speeds
in revolutions per minute (rpm). Red range
indicates propeller overspeed warning; a white
high-rpm range indicates above normal operating
speeds (Models 172S, 206H, and T206H)

Fuel Flow Indicator (FFLOW GPH) – Shows
the current fuel ﬂow in gallons per hour (gph).
For turbocharged aircraft, the indicator displays
a small stand-alone green band indicating
maximum takeoff fuel ﬂow. A white tick mark
indicates the maximum cruise fuel ﬂow (Model
T182T only).

Oil Pressure Indicator (OIL PRES) – Displays
pressure of the oil supplied to the engine in
pounds per square inch (psi).

Oil Temperature Indicator (OIL TEMP)
– Displays the engine oil temperature in degrees
Fahrenheit (°F).

Cylinder Head Temperature Indicator (CHT)
Models 182T, T182T, 206H, T206H – Shows
the head temperature of the hottest cylinder
(number shown in triangular pointer) in degrees
Fahrenheit (°F).

Exhaust Gas Temperature Indicator (EGT)
Normally-aspirated Aircraft – Displays the
exhaust gas temperature of the hottest cylinder
(number shown in triangular pointer) in degrees
Fahrenheit (°F).

Turbine Inlet Temperature Indicator (TIT)
Turbocharged Aircraft – Displays the temperature
at the turbine inlet in degrees Fahrenheit (°F).

Vacuum Pressure Indicator (VAC) Models
172R and 172S – Displays vacuum pressure.

NOTE: Refer to the Pilot’s Operating Handbook
(POH) for limitations.

EIS information is presented in three displays, accessed
using the ENGINE Softkey on the MFD:
• Engine Display – Default display, shows all critical
engine, fuel, and electrical indicators
• Lean Display – Provides engine leaning
information
• System Display – Shows numeric readouts of
critical engine, fuel, and electrical indicators
Green and white bands indicate normal ranges of
operation; yellow and red bands indicate caution and
warning, respectively. If sensory data to an instrument
becomes invalid or unavailable, a red “X” is shown across
the instrument.

3.1

ENGINE DISPLAY

The Engine Display is the default EIS display and can
be displayed after viewing other EIS displays by pressing
the ENGINE Softkey.
The EIS automatically defaults back to the Engine
Display from the Lean or System Display when certain
parameters are exceeded. Fluctuations in engine speed
and fuel quantity above certain levels, depending on the
airframe, also cause reversion back to the Engine Display.
1

Engine Manifold Pressure Gauge (MAN IN)
Models 182T, T182T, 206H, T206H – Displays
engine power in inches of mercury (in Hg).
Turbocharged aircraft have a red portion of the
gauge indicating the maximum manifold pressure
range. A white tick mark is displayed indicating
the cruise manifold pressure (Model T182T only).

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

3-1

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
10

Fuel Quantity Indicator (FUEL QTY GAL)
– Shows the quantity of fuel in the tanks, in
gallons, ranging from zero to full (F) for each fuel
tank (left–L and right–R). When full, the indicator
displays to 35 gallons per side (26 gallons for the
Models 172R and 172S).

Voltmeter (M, E BUS VOLTS) – Displays the
main and essential bus voltages.

Ammeter (M, S BATT AMPS) – Shows the
main and standby battery load in amperes.

Engine Hours (Tach) (ENG HRS) Models 172R
and 172S – A numeric readout gives the time (in
hours) the engine has been in service.

Model 172R

Model 172S

Model 182T

Model 206H

Figure 3-1 Engine Display (Normally-aspirated Aircraft)
3-2

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
Cruise
Manifold
Pressure

Cruise
Fuel Flow

Model T182T

Maximum
Takeoff Fuel
Flow

Model T206H

Figure 3-2 Engine Display (Turbocharged Aircraft)

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

3-3

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)

3.2

LEAN DISPLAY

for the selected cylinder to be displayed below
the indicator.

NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in
the Pilot’s Operating Handbook (POH).

3-4

Fuel Flow (FFLOW GPH) – Shows the current
fuel ﬂow in gallons per hour (gph).

Turbine Inlet Temperature Indicator
(TIT) Models T182T and T206H – Displays
the temperature at the turbine inlet in degrees
Fahrenheit (°F). When the ASSIST Softkey is
pressed, the TIT deviation from peak (∆PEAK) is
displayed below the indicator.

Exhaust Gas Temperature Bar Graph (EGT
°F) – Displays the exhaust gas temperature of all
cylinders in degrees Fahrenheit (°F); a readout
for the selected cylinder (by default, the hottest
cylinder) is shown below the bar graph. The
selected cylinder is indicated in light blue.
Cylinders whose EGTs are in the normal range
appear in white. Pressing the ASSIST Softkey
causes the EGT deviation from peak (∆PEAK)

Cylinder Head Temperature Indicator (CHT)
– Shows the head temperatures of all cylinders
in degrees Fahrenheit (°F); a readout for the
selected cylinder (by default, the hottest cylinder)
is shown below the bar graph. The selected
cylinder is indicated in light blue. Cylinders
whose CHTs are in the normal range appear in
white. Cylinders whose CHTs enter the caution
and warning ranges appear in yellow and red,
respectively.

Fuel Quantity Indicator (FUEL QTY GAL)
– Shows the quantity of fuel in the left and right
fuel tanks (left–L and right–R). When full, the
indicator displays to 35 gallons per side (26
gallons for the Models 172R and 172S).

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)

Hollow Block
Represents
Peak

5
5

Model 172R

Model 172S

Model 182T

Model 206H

Figure 3-3 Lean Display (Normally-aspirated Aircraft)

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

3-5

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
Cruise
Manifold
Pressure

Model T182T

Model T206H

Figure 3-4 Lean Display (Turbocharged Aircraft)

The Lean Display is accessed by pressing the ENGINE
Softkey followed by the LEAN Softkey and provides
information for performing engine leaning.

3-6

From the Lean Display, the pilot can utilize the CYL
SLCT and ASSIST softkeys to obtain information about
speciﬁc cylinders. Pressing the CYL SLCT (Cylinder
Select) Softkey cycles through the cylinders (i.e., changes
the cylinder indicated on the bar graphs in light blue).
This softkey is disabled when the ASSIST Softkey is
pressed or when a cylinder experiences a caution or
warning condition; the softkey remains disabled until the
temperature returns to normal.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
The ASSIST Softkey aids in the leaning process by
identifying the peak of the ﬁrst cylinder whose temperature
falls. If the temperature of the peaked cylinder exceeds
the peak value, the peak value is not updated. Press the
ASSIST Softkey to stop peak monitoring.

Normally-aspirated Aircraft
For normally-aspirated aircraft, when a cylinder peaks,
its peak is represented by a hollow block on the EGT Bar
Graph. The EGT readout for the peaked cylinder, indicated on the bar graph in light blue, appears directly beneath
the bar graph. The system automatically switches to the
ﬁrst peak obtained and displays the temperature deviation
from peak (∆PEAK) in degrees Fahrenheit (°F) below the
EGT readout.

Turbocharged Aircraft
Leaning for turbocharged aircraft is done with reference to the Turbine Inlet Temperature (TIT). When the
temperature peaks, the numeric readout (∆PEAK) appears
below the TIT Indicator and displays the difference between peak and current TITs, in degrees Fahrenheit (°F).
If a peak is not displayed, underscores are shown until
one is established.

3.3

The System Display is accessed by pressing the
ENGINE Softkey followed by the SYSTEM Softkey and
shows critical engine, fuel, and electrical parameters.
Fuel calculations are based on the fuel ﬂow totalizer
and the displayed fuel remaining, adjusted by the pilot
using the following softkeys:
• RST FUEL – Resets totalizer-based fuel remaining
(GAL REM) to zero and the fuel used (GAL USED)
to zero
• GAL REM – Gives access to softkeys for adjusting
the amount of fuel remaining for purposes of fuel
calculations
Fuel remaining can be adjusted in one or ten-gallon
increments using the appropriate softkeys. Softkeys also
allow entering the full tank quantity for the aircraft or the
tab quantity, which is 35 gallons (Models 172R and 172S)
or 64 gallons (Models 182T, T182T, 206H, and T206H).

SYSTEM DISPLAY
NOTE: Fuel calculations do not use the aircraft
fuel quantity indicators and are calculated from
the last time the fuel was reset.
NOTE: The pilot should refer to the Pilot’s
Operating Handbook (POH) for fuel values and
limitations. The displayed fuel remaining can be
adjusted up to 53 gal (Models 172R, 172S) or 87
gal (Models 182T, T182T, 206H, T206H).

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

3-7

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)

3-8

Engine Manifold Pressure Gauge (MAN IN)
Models 182, T182, 206, T206 – Displays engine
power in inches of mercury (in Hg). Turbocharged
aircraft have a red portion of the gauge indicating
the maximum manifold pressure range. A white
tick mark is displayed indicating the cruise
manifold pressure (Model T182 only).

Oil Pressure (OIL PSI) – Displays pressure
of the oil supplied to the engine in pounds per
square inch (psi).

Oil Temperature (OIL °F) – Displays the engine
oil temperature in degrees Fahrenheit (°F).

Engine Hours (Tach) (ENG HRS) Models 182,
T182, 206, T206 – A numeric readout gives the
time (in hours) the engine has been in service.

Vacuum Pressure Indicator (VAC) Models 182,
T182, 206, T206 – Displays vacuum pressure.

Fuel Flow (FFLOW GPH) – Shows the current
fuel ﬂow in gallons per hour (gph).

Calculated Fuel Used (GAL USED) – Shows
quantity of fuel used in gallons based on fuel ﬂow
since last reset.

Set Fuel Remaining (GAL REM) – Shows
current fuel remaining in gallons as set by the
pilot and adjusted for fuel burn since last set.

Voltmeter (M, E BUS VOLTS) – Displays the
main and essential bus voltages.

Ammeter (M, S BATT AMPS) – Shows the
main and standby battery load in amperes.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
2

Model 172R

Model 172S

Model 182T

Model 206H

Figure 3-5 System Display (Normally-aspirated Aircraft)

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

3-9

SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)

Cruise
Manifold
Pressure

Model T182T

Model T206H

Figure 3-6 System Display (Turbocharged Aircraft)

3-10

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 4 – NAV/COM &
TRANSPONDER

SECTION 4: NAV/COM AND
TRANSPONDER
The NAV/COM controls and frequency boxes share the
same locations on the on the Primary Flight Display and
the Multi-Function Display.

NAV
Controls

NAV Frequency Box

COM Frequency Box

Figure 4-1 G1000 VHF NAV/COM Interface (PFD shown)

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

COM
Controls

DME Tuning Window

4-1

SECTION 4 – NAV/COM &
TRANSPONDER
Standby NAV
Frequency Field

Tuning Box

Selected COM
Frequency

Selected NAV
Frequency

Figure 4-2 Frequency Fields

Active NAV
Frequency Field

Frequency Transfer Arrow

Active COM
Frequency Field

Standby COM
Frequency Field

Tuning Box

Figure 4-3 Frequency Transfer Arrow and Tuning Box

NAV Controls

COM Controls
VOL/PUSH
ID Knob

VOL/PUSH
SQ Knob

Frequency Transfer Key

Dual NAV
Knob

Dual COM
Knob

• Turn to tune in desired
frequencies.
• Press to change tuning box
positions.
Figure 4-4 NAV/COM Controls

4-2

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 4 – NAV/COM &
TRANSPONDER

4.1

RADIO STATUS INDICATIONS

Squelch
Indication

• RX – When a COM signal is received, a white ‘RX’
appears by the active COM frequency during signal
reception.

Figure 4-7 Squelch Indication

• TX – When a COM radio is transmitting, a white ‘TX’
indication appears to the right of the corresponding
COM frequency.

4.4

• ID – When the Morse code identiﬁer is ON for a
NAV radio, a white ‘ID’ indication appears to the
left of the corresponding active NAV frequency.
The Morse code identifier can be heard if the
corresponding NAV radio is selected on the audio
panel.

4.5

Figure 4-5 Radio Status Indications

4.2

QUICKLY ACTIVATING 121.500 MHZ

Pressing and holding the COM Frequency Transfer
Key for approximately two (2) seconds automatically tunes
the selected COM radio to the emergency frequency.

OPTIONAL NAV RADIOS

DME Radio (optional)
The DME Tuning Window is displayed by pressing the
DME Softkey.

VOLUME

‘VOLUME’ is displayed in place of the associated radio
name (i.e., ‘COM1’ or ‘NAV2’) for two seconds after the
volume level is last changed. The percentage of maximum
volume is displayed in place of the standby frequency
selected by the tuning box.

Figure 4-8 Radio Tuning Window

Changing the DME tuning source:
Figure 4-6 COM Volume Level

4.3

AUTOMATIC SQUELCH

Automatic squelch can be disabled for a COM radio by
pressing the COM Knob to place the tuning box on the
desired COM’s standby frequency, then by pressing the
VOL/PUSH SQ Knob.
When Automatic Squelch is disabled, a white ‘SQ’
appears next to the COM frequency.
190-00384-08 Rev. A

1) From the tuning window, turn the large FMS Knob
to highlight the DME source ﬁeld.
2) Turn the small FMS Knob to display the selection
window. Turn the FMS Knob to select the desired
mode and press the ENT Key.

Figure 4-9 DME Selection Window

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

4-3

SECTION 4 – NAV/COM &
TRANSPONDER

4.7

ADF Radio (optional)
The G1000 does not support tuning of the ADF in
Nav III aircraft. ADF tuning is accomplished through the
Bendix/King KR 87 ADF Radio. ADF volume must also be
adjusted through the KR 87.

4.6

FREQUENCY AUTO-TUNING

TRANSPONDER

Mode Selection
The STBY, ON, ALT, GND, VFR, CODE, and IDENT
Softkeys can be accessed by pressing the XPDR Softkey.
Ground Mode (Automatic or Manual)
GND is displayed when the aircraft is on the ground or
when the GND Softkey is pressed. The transponder does
not allow Mode A and Mode C replies, but it does permit
acquisition squitter and replies to discretely address
Mode S interrogations.

Auto-tuning on the PFD

Figure 4-11 Ground Mode
Figure 4-10 Nearest Airports Window (PFD)

1) Press the NRST Softkey to display the Nearest
Airports Window.
2) Turn either FMS Knob to highlight the desired
frequency.

Standby Mode (Manual)
Press the STBY Softkey. In Standby Mode, the transponder does not reply to interrogations, but new codes
can be entered.
STBY Mode (White
Code Number and
Mode)

3) Press the ENT Key to place the frequency in the
standby ﬁeld of the active COM.
4) Press the Frequency Transfer Key to place the
frequency in the active ﬁeld.
NAV frequencies are entered automatically in the
NAV frequency active or standby ﬁeld (depending in CDI
selection) upon approach loading or approach activation.

Auto-tuning on the MFD
Auto-tuning on the MFD is done in much the same way
as on the PFD. Use the FMS Knobs to select the desired
frequency on any of the information pages. Pressing the
ENT Key then loads the selected frequency in the tuning
box as a standby frequency.
4-4

Figure 4-12 Standby Mode

Manual ON Mode
Press the ON Softkey. ON Mode generates Mode A
and Mode S replies, but Mode C altitude reporting is inhibited.
ON Mode
(No Altitude
Reporting)

Figure 4-13 ON Mode

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 4 – NAV/COM &
TRANSPONDER
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.
All transponder replies requesting altitude information
are provided with pressure altitude information.
ALT Mode (Mode C
Altitude Reporting)

Figure 4-14 Altitude Mode

Reply Status
When the transponder sends replies to interrogations,
an “R” indication appears momentarily in the reply status
ﬁeld.
Reply
Indication

Figure 4-15 Reply Indication

Enter Code Using Softkeys
1) Press the XPDR Softkey to display the transponder
Mode Selection softkeys.
2) Press the CODE Softkey to display the transponder
Code Selection softkeys, which includes the digit
softkeys.
3) Press the appropriate digit softkeys to enter the
code in the four-digit code ﬁeld of the Transponder
Status Box. When the last digit is entered, the
transponder code becomes active.
When entering a code, press the BKSP Softkey as
needed to back up and change code digits.

Enter Code Using the FMS Knob
1) Press the XPDR Softkey to display the transponder
Mode Selection softkeys.
2) Press the CODE Softkey to display the transponder
Code Selection softkeys, which includes the digit
softkeys.
3) Turn the small FMS Knob to enter the ﬁrst two
digits.
4) Turn the large FMS Knob to place the cursor in
position to change the second two digits.

Code Selection
VFR Code Selection
1) Press the XPDR Softkey to display the transponder
Mode Selection softkeys.
2) Press the VFR Softkey to enter the VFR code.
Pressing the VFR Softkey again restores the previous
identiﬁcation code.

5) Turn the small FMS Knob to enter the second two
digits.
6) Press the ENT Key to activate the code immediately,
or wait 10 seconds and the code will become
active.

NOTE: The pre-programmed VFR Code is set at
the factory to 1200.

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

4-5

SECTION 4 – NAV/COM &
TRANSPONDER

Flight ID Reporting
If so conﬁgured, the Flight ID may be entered in the
Timer/Reference Window.

Flight ID

Figure 4-16 Timer/References Window

1) Press the TMR/REF Softkey to display the Timer/
References Window.
2) Turn the large FMS Knob to place the cursor in the
Flight ID ﬁeld.
3) Turn the small FMS Knob to enter the desired ﬁrst
character.
4) Turn the large FMS Knob to place the cursor in the
next desired ﬁeld.
5) Turn the small FMS Knob to enter the next desired
character.
6) Repeat steps 4 and 5 until the desired Flight ID is
entered.
7) Press the ENT Key. ‘updating’ is displayed as the
Flight ID is loaded into the system.

4-6

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 5 – AUDIO PANEL

SECTION 5: AUDIO PANEL

Transmitters

Receiver Audio

Disabled

Passenger Address
(Disabled on 172R/S)

Cabin Speaker

Marker Beacon/Mute

Marker Beacon Signal Sensitivity

Aircraft Navigation Radio Audio
(Optional, disabled if ADF and/or DME
are not installed)

Aircraft Navigation Radio Audio

Disabled
Manual Squelch

Digital Clearance Recorder Play Key
ICS Isolation

VOL/SQ
VOL Annunciation

SQ Annunciation
Reversionary Mode

Figure 5-1 Front Panel Controls

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

5-1

SECTION 5 – AUDIO PANEL

5.1

COM RADIO SELECTION

Pressing the COM1 MIC or COM2 MIC Key selects
the active transmitter (i.e., microphone). The associated
receiver audio (COM1 or COM2) also becomes selected
when the COM MIC Key is pressed.
To prevent deselecting the desired received audio
when pressing another COM MIC Key, press the already
selected COM1 or COM2 Key before pressing the other
COM MIC Key.

Figure 5-2 Transceivers

5.2

CABIN SPEAKER

Pressing the SPKR Key selects and deselects the cabin
speaker. All of the radios can be heard over 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.

Talk (PTT) must be pressed to deliver PA announcements.
The PA Annunciator ﬂashes about once per second while
the PTT is depressed.

5.4

MARKER BEACON RECEIVER

The marker beacon receiver is always on. Only the
marker beacon audio can be turned off. Figure 5-4 shows
the marker beacon annunciators on the PFD.
When the MKR/MUTE Key is pressed, the key annunciator is lit and the audio tone can be heard over the
speaker or headsets during marker beacon reception.
When the tone is active, pressing the MKR/MUTE Key
once mutes the audio but does not affect the marker annunciator. The audio returns when the next marker signal
is received.
To turn off the marker beacon audio, press the MKR/
MUTE Key once when there is no marker indication present, or press twice when an indication is present. The key
annunciator extinguishes when the marker beacon audio
is turned off.
Outer Marker

Middle Marker

Figure 5-3 Passenger Address and Speaker Keys

5.3

PASSENGER ADDRESS (PA) SYSTEM
(T)182T AND (T)206H ONLY

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-to5-2

Inner Marker

Altimeter

Figure 5-4 Marker Beacon Annunciators on the PFD

Marker Beacon Signal Sensitivity
The HI SENS Key can be pressed for increased marker
beacon signal sensitivity.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 5 – AUDIO PANEL

5.6

Press the PILOT and/or COPLT Key to select who
is isolated from hearing the Nav/Com radios and music.
Selection scenarios are addressed in Table 5-1.

Figure 5-5 Marker Beacon

5.5

INTERCOM SYSTEM (ICS) ISOLATION

NAV RADIO AUDIO SELECTION

Pressing DME, ADF, NAV1, or NAV2 selects and
deselects the audio source and activates the annunciator.
Selected audio can be heard over the headset and the
speakers. These four keys can be selected individually
or together.

Figure 5-7 ICS Isolation

Figure 5-6 Navigation Radios

PILOT KEY
Annunciator

COPLT KEY
Annunciator

Pilot Hears

Copilot Hears

Passenger Hears

OFF

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

Copilot, passengers, music

OFF

Selected radios,
aural alerts, pilot,
passengers, music

Copilot

Selected radios, aural alerts,
pilot, passengers, music

Selected radios, aural
alerts, pilot, copilot

Passengers, music

Table 5-1 ICS Isolation Modes
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

5-3

SECTION 5 – AUDIO PANEL

5.7

INTERCOM SQUELCH CONTROL

Select manual squelch for intercom audio by pressing
the MAN SQ Key to light the annunciator.
Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL
or SQ respectively.

• Pressing the MKR/MUTE Key while playing a
memory block stops play.
• Pressing the PLAY Key during play begins playing
the previously recorded memory block. Each
subsequent press of the PLAY Key begins playing
the next previously recorded block.
If a COM input signal is detected while playing, play
is halted and the new COM input signal is recorded as the
latest block.

Figure 5-8 Volume/Squelch Control

5.8

DIGITAL CLEARANCE RECORDER
AND PLAYER

Each reception of primary active COM audio is
automatically recorded in a memory block. When the next
transmission is received, it is recorded in the next memory
block, and so on. Once the 2.5 minutes of recording time
has been reached, the recorder begins recording over the
stored memory blocks, starting from the oldest block.
Powering off the unit automatically clears all recorded
blocks.

Figure 5-9 Clearance Recorder Play Key

• Pressing the PLAY Key once plays the latest recorded
memory block, then returns to normal operation.

5-4

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

SECTION 6: AUTOMATIC FLIGHT
CONTROL
NOTE: The Aircraft Flight Manual (AFM) always
supersedes the information in this guide. This
section only applies to the GFC 700 Automatic
Flight Control System (AFCS).

6.1

AFCS CONTROLS

The following dedicated AFCS keys are located on the
bezels of the PFD and MFD:

acknowledge an autopilot disconnect and mute the
associated aural tone.
• CWS Button (Control Wheel Steering)
Momentarily disengages the autopilot 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). The CWS
Button is located on the top of the pilot’s control
wheel right grip. Upon release of the CWS
Button, the ﬂight director may establish new
reference points, depending on the current
pitch and roll modes.
• GA Switch (Go-Around)
Disengages the autopilot, selects ﬂight director GoAround Mode, and activates the missed approach.
The GA Switch is located on the instrument
panel above the throttle.
• MET Switch (Manual Electric Trim)

Figure 6-1 Dedicated AFCS Controls

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. The red AP DISC Switch is located
forward of the MET Switch on the pilot’s control
wheel left grip. This switch may be used to
190-00384-08 Rev. A

The MET Switch is located on the pilot’s control
wheel left grip. 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 MET
ARM switch can be used to disengage the autopilot
and to acknowledge an autopilot disconnect alert
and mute the associated aural tone. 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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-1

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

6.2

FLIGHT DIRECTOR OPERATION

With the ﬂight director activated, the aircraft can be
hand-ﬂown to follow the path shown by the Command
Bars. Maximum commanded pitch (+20°/-15°) and bank
(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
Pressing the FD or AP Key (when the ﬂight director is
not active) activates the ﬂight director in default pitch/roll
modes. Pushing the GA Switch or any ﬂight director mode
key activates the ﬂight director in the respective mode(s).
Roll Modes

Armed

Active

The ﬂight director may be turned off by pressing the
FD Key.

Command Bars
Upon activation of the ﬂight director, Command Bars
are displayed on the PFD as a single cue. If the attitude
information sent to the ﬂight director becomes invalid or
unavailable, the Command Bars are removed from the
display. The Command Bars do not override the aircraft
symbol.

Figure 6-2 Command Bars

Autopilot
Status

Pitch Modes

Active

Mode
Reference

Armed

AFCS Status Box

Selected Altitude

Command Bars

Selected Heading

Selected Course

GPS is Selected
Navigation Source

Figure 6-3 PFD AFCS Display
6-2

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

AFCS Status Box
Flight director roll modes are shown on the left and
pitch on the right. Armed modes are annunciated in
white and active in green. Autopilot status is displayed in
the center of the AFCS Status Box.

6.3

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).
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 ten
seconds.
A ﬂashing yellow mode annunciation and annunciator
light indicate loss of sensor (AHRS, ADC, IAU) or
navigation data (VOR, LOC, GPS, VNAV, WAAS) required
to compute commands. When such a loss occurs, the
system automatically begins to roll the wings level or
maintain the pitch angle, 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 ten seconds no action is taken, the ﬂashing
annunciation stops and the ﬂight director enters the
default mode for the affected axis.
Figure 6-4 Loss of VOR Signal

190-00384-08 Rev. A

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.
The ﬂight director is automatically disabled if the attitude
information required to compute the default ﬂight director
modes becomes invalid or unavailable.

Pitch Modes
• Pitch Hold (default mode)— Holds the current
aircraft pitch attitude; may be used to climb/descend
to the Selected Altitude
• Selected Altitude Capture — Captures the
Selected Altitude
• Altitude Hold — Holds the current Altitude
Reference
• Vertical Speed — Maintains the current aircraft
vertical speed; may be used to climb/descend to the
Selected Altitude
• Flight Level Change — Maintains the current
aircraft airspeed while the aircraft is climbing/
descending to the Selected Altitude
• Vertical Path Tracking — Follows an active
vertical proﬁle for enroute and terminal phases of
ﬂight
• VNAV Target Altitude Capture — Captures the
VNAV Target Altitude
• Glidepath — Intercepts and tracks the WAAS
glidepath on approach (only available in installations
with GIA 63W Integrated Avionics Units and when
WAAS is available)
• Glideslope — Intercepts and tracks the ILS
glideslope on approach
• Go Around — Automatically disengages the
autopilot and commands a constant pitch angle and
wings level while in the air

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-3

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Table 6-1 lists the pitch modes with their corresponding
controls and annunciations. The mode reference (shown
with default measurement units) 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 pitch mode
reference while operating under Pitch Hold, Vertical
Speed, or Flight Level Change Mode.

Pitch Mode
Pitch Hold
Selected Altitude Capture

Control

Annunciation

Reference Range

(default)

PIT

-20° to +15°

Reference
Change
Increment
0.5°

ALTS

Altitude Hold

ALT Key

ALT

nnnnn FT

Vertical Speed
Flight Level Change, IAS
Hold
Vertical Path Tracking
VNAV Target Altitude
Capture
Glidepath

VS Key

nnnn FPM

-3000 to +1500 fpm

100 fpm

FLC Key

FLC

nnn KT

70 to 165 kt

1 kt

Glideslope
Go Around (in air)

VNV Key

VPTH

ALTV

APR Key
GA Switch

GP
GS
GA

* 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 VNAV Target Altitude.
** ALTV is armed automatically under VPTH when the VNAV Target Altitude is to be captured instead of
the Selected Altitude.
Table 6-1 Flight Director Pitch Modes

6-4

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Pitch Hold Mode (PIT)

Changing the Pitch Reference

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 the mode is activated.

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

In Pitch Hold Mode, the ﬂight director maintains a
constant pitch attitude, the pitch reference. The pitch
reference is set to the aircraft 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.
Pitch Hold Mode Active

Selected Altitude Capture
Mode Armed

Selected
Altitude

Command Bars Maintain Desired Pitch
Reference

Figure 6-5 Pitch Hold Mode

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-5

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Selected Altitude Capture Mode (ALTS)
Selected Altitude Capture Mode arms automatically
when the ﬂight director is in Pitch Hold, Vertical Speed,
Flight Level Change, or Go Around Mode. This mode
is also armed automatically under Vertical Path Tracking
Mode when the Selected Altitude is to be captured
instead of the VNAV Target Altitude. The white ‘ALTS’
annunciation indicates Selected Altitude Capture Mode is
armed (see Figure 6-5 for example).
The ALT Knob is used to set the Selected Altitude,
shown above the Altimeter until Selected Altitude Capture
Mode becomes active.
As the aircraft nears the Selected Altitude, the ﬂight
director automatically transitions to Selected Altitude
Capture Mode with Altitude Hold Mode armed (Figure
6-7). This automatic transition is indicated by the green
‘ALTS’ annunciation ﬂashing for up to ten seconds and the
appearance of the white ‘ALT’ annunciation. The Selected
Altitude is shown as the Altitude Reference beside the
‘ALTS’ annunciation.
At 50 ft 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 ten seconds
to indicate the automatic transition.
Altitude Reference (In
This Case, Equal to
Selected Altitude)

Flash Up to 10 sec, Indicating Automatic Transition

Figure 6-6 Automatic Mode Transitions During Altitude Capture

6-6

Changing the Selected Altitude
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.
Altitude Hold Mode (ALT)
Altitude Hold Mode can be activated by pressing the
ALT Key; the ﬂight director maintains the current aircraft
altitude (to the nearest ten feet) as the Altitude Reference.
The ﬂight director’s Altitude Reference is shown in the
AFCS Status Box and 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.
Selected Altitude Capture Mode automatically transitions
to Altitude Hold Mode when the altitude error is less than
50 ft. In this case, the Selected Altitude becomes the ﬂight
director’s Altitude Reference.
Changing the Altitude Reference
NOTE: Turning the ALT Knob while in Altitude
Hold Mode changes the Selected Altitude, but
not the ﬂight 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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
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.

Altitude Hold
Mode Active

Flight Director Altitude Reference

Selected Altitude
Selected Altitude Bug

Command Bars Hold
Pitch Attitude to Maintain Altitude Reference

Figure 6-7 Altitude Hold Mode

Vertical Speed Mode (VS)
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. Vertical Speed Mode does not consider
the relative position of the Selected Altitude in relation to
the current aircraft altitude at the time of mode activation,
so it is possible to use Vertical Speed Mode while not
climbing/descending to the Selected Altitude.

190-00384-08 Rev. A

Vertical Speed Mode is activated by pressing the VS
Key; the ‘VS’ annunciation appears in the AFCS Status Box
to indicate the active pitch mode, along with the Vertical
Speed Reference to the right. 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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-7

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Vertical Speed
Mode Active

Vertical Selected Altitude Capture
Speed
Mode Armed
Reference
Selected Altitude
Vertical Speed
Reference
Vertical Speed
Reference Bug

Command Bars
Indicate Climb
to Attain Vertical
Speed

Figure 6-8 Vertical Speed Mode

Changing the Vertical Speed Reference
The Vertical Speed Reference (shown both in the AFCS
Status Box and above/below the Vertical Speed Indicator)
may be changed by:
• Using the NOSE UP/NOSE DN Keys
• By pressing the CWS Button, hand-flying the
aircraft to attain a new Vertical Speed Reference,
then releasing the CWS Button
Flight Level Change Mode (FLC)
NOTE: The Selected Altitude should be set before
selecting Flight Level Change Mode.

6-8

Flight Level Change Mode is selected by pressing the
FLC Key. When Flight Level Change Mode is active, the
ﬂight director continuously monitors Selected Altitude,
airspeed, and altitude. This mode acquires and maintains
the Airspeed Reference while climbing or descending to
the Selected Altitude (shown above the Altimeter). The
Airspeed Reference is set to the current airspeed upon
mode activation. Flight Level Change Mode is indicated
by an ‘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.
Engine power must be adjusted to allow the autopilot
to ﬂy the aircraft at a pitch attitude corresponding to the
Airspeed Reference and the desired ﬂight proﬁle (climb or

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
descent). 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.
Changing the Airspeed Reference
The Airspeed Reference (shown in both the AFCS
Status Box and above the Airspeed Indicator) may be
adjusted:
• Using the NOSE UP/NOSE DN Keys
• By pressing the CWS Button, hand-ﬂying the aircraft
to a new airspeed, then releasing the CWS Button
to establish the new Airspeed Reference

Flight Level Change
Mode Active

Airspeed Altitude Hold
Reference Mode Armed

Airspeed Reference
Airspeed Reference Bug

Figure 6-9 Flight Level Change Mode
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-9

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Vertical Navigation Modes (VPTH, ALTV)
NOTE: Pressing the CWS Button while Vertical
Path Tracking Mode is active does not cancel
the mode. The autopilot guides the aircraft back
to the descent path upon release of the CWS
Button.
NOTE: VNAV ﬂight director pitch modes are
available only in conjunction with GPS roll
modes.
NOTE: The Selected Altitude takes precedence
over any other vertical constraints.

Vertical Navigation (VNAV) ﬂight control is available
for enroute/terminal cruise and descent operations when
VNAV has been enabled and a VNAV ﬂight plan (with at
least one vertical waypoint) or direct-to with a vertical
constraint has been activated. Refer to the Navigation
section for more information on VNAV ﬂight plans. The
ﬂight director may be armed for VNAV 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 VNAV 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 VNAV ﬂight plan, the ﬂight director
transitions to Altitude Hold Mode and cancels any armed
VNAV modes.

When a vertical proﬁle (VNAV 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 VNAV
Target Altitude (ALTV) or the Selected Altitude (ALTS),
whichever is greater.

Figure 6-10 Vertical Path Tracking Armed Annunciations

Prior to descent path interception, the Selected Altitude
must be set below the current aircraft altitude by at least
75 ft. For the ﬂight director to transition from Altitude
Hold to Vertical Path Tracking Mode, acknowledgment is
required within ﬁve minutes of descent path capture by:
• Pressing the VNV Key
• Adjusting the Selected Altitude
If acknowledgment is not received within one minute of
descent path interception, the white ‘VPTH’ annunciation
and the VNV Key annunciator light start 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 Mode (VPTH)
NOTE: If another pitch mode key is pressed while
Vertical Path Tracking Mode is selected, Vertical
Path Tracking Mode reverts to armed.
6-10

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
In conjunction with the “TOD [top of descent] within 1
minute” annunciation in the Navigation Data Box, VNAV
indications (VNAV Target Altitude, vertical deviation, and
vertical speed required) appear on the PFDs in magenta
(Figure 6-11).
Altitude Hold Mode Active

Vertical Path Tracking Armed, (Flashing Indicates Acknowledgment Required)
VNAV Target
Altitude
Selected Altitude Below
VNAV Target
Vertical Deviation
Indicator
Required Vertical
Speed Bug

Enroute Phase of
Flight

HSI Set to GPS

Figure 6-11 Vertical Path Capture

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6-11

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
When a descent leg is captured (Figure 6-12), Vertical
Path Tracking becomes active and tracks the descent proﬁle. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed
as appropriate.

Vertical Path Tracking Active

VNAV Target Altitude Capture Armed
VNAV
Target
Altitude

Vertical
Deviation
Indicator
Required
Vertical
Speed Bug

Terminal
Phase of
Flight

HSI Set to GPS

Figure 6-12 Vertical Path Tracking Mode

Automatic Pitch Hold Reversion
Several situations can occur while Vertical Path
Tracking Mode is active which cause the ﬂight director to
revert to Pitch Hold Mode. Vertical Path Tracking and the
appropriate altitude capture modes are armed for possible
descent proﬁle recapture if the vertical deviation:
• Exceeds 200 ft during an overspeed condition
• Experiences a discontinuity exceeding 200 ft due to
a ﬂight plan change
• Becomes invalid due to excessive cross-track error,
track angle error
• Cannot be computed for a leg type (such as a hold
or procedure turn)
6-12

The following circumstances cause mode reversion
without arming Vertical Path Tracking Mode:
• Navigation source manually changed from GPS
• CNCL VNV Softkey selected on the Active Flight
Plan Page (MFD)
• All remaining vertical waypoints deleted from the
ﬂight plan
• Displays entering Reversionary Mode
Non-Path Descents
Pitch Hold, Vertical Speed, and Flight Level Change
modes can also be used to ﬂy non-path descents while

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
VNAV 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 recapture.
Figure 6-13 Flight Level Change VNAV Non-Path Descent

To prevent immediate proﬁle re-capture, the following
must be satisﬁed:
• At least ten seconds have passed since the non-path
transition was initiated
• Vertical deviation from the proﬁle has exceeded 250
ft, but is now less than 200 ft
Pressing the VNV Key twice re-arms Vertical Path
Tracking for immediate proﬁle re-capture.
VNAV Target Altitude Capture Mode (ALTV)
NOTE: Armed VNAV Target Altitude and Selected
Altitude capture modes are mutually exclusive.
However, Selected Altitude Capture Mode is
armed implicitly (not annunciated) whenever
VNAV Target Altitude Capture Mode is armed.
This ensures the Selected Altitude is not violated
during a change from VNAV Target Altitude
Capture to Selected Altitude Capture Mode close
to Selected Altitude interception.

VNAV Target Altitude Capture is analogous to Selected
Altitude Capture Mode and is armed automatically
after the VNV Key is pressed and the next VNAV Target
Altitude is to be intercepted before the Selected Altitude.
The annunciation ‘ALTV’ indicates that the VNAV Target
Altitude is to be captured. VNAV 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 Navigation section for details). At the same time as
190-00384-08 Rev. A

“TOD within 1 minute” is annunciated in the Navigation
Data Box, the VNAV Target Altitude is displayed above the
Vertical Speed Indicator (see Figure 6-12). VNAV Target
Altitudes can be modiﬁed until VNAV Target Altitude
Capture Mode becomes active.
As the aircraft nears the VNAV Target Altitude, the
ﬂight director automatically transitions to VNAV Target
Altitude Capture Mode with Altitude Hold Mode armed.
This automatic transition is indicated by the green ‘ALTV’
annunciation ﬂashing for up to ten seconds and the
appearance of the white ‘ALT” annunciation. The VNAV
Target Altitude is shown as the Altitude Reference beside
the ‘ALTV’ annunciation.
At 50 ft from the VNAV Target Altitude, the ﬂight
director automatically transitions from VNAV 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 pitch mode
ﬁeld and ﬂashes green for ten seconds to indicate the
automatic transition. The ﬂight director automatically
arms Vertical Path Tracking, allowing upcoming descent
legs to be captured and subsequently tracked.
Altitude Reference (In This
Case, Equal To VNAV
Altitude Target)

Flash up to 10 sec, Indicating Automatic Transition

Figure 6-14 VNAV Altitude Capture

Changing the VNAV Target Altitude
NOTE: Pressing the CWS Button while in VNAV
Target Altitude Capture Mode does not cancel
the mode.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-13

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Changing the current VNAV Target Altitude while
VNAV 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 VNAV Target
Altitude or the Selected Altitude, depending on which
altitude is to be intercepted ﬁrst.
VNAV target altitudes can be changed while editing the
active ﬂight plan (see the Navigation section for details).
Glidepath Mode (GP)
NOTE: Pressing the CWS Button while Glidepath
Mode is active does not cancel the mode. The
autopilot guides the aircraft back to the glidepath
upon release of the CWS Button.
GPS Approach Mode Active

NOTE: Glidepath Mode is available only in
installations with GIA 63W Integrated Avionics
Units and WAAS currently available.

Glidepath mode is used to track the WAAS-based
glidepath. Arming Glidepath Mode (annunciated in white
as ‘GP’) requires:
• Approach supporting WAAS vertical guidance is
loaded into the ﬂight plan
• Expected availability of vertical guidance
• GPS Approach Mode is armed, after acquiring
clearance for approach, prior to intercepting the
WAAS glidepath (GPS is the selected navigation
source and the APR Key is pressed; see GPS
Approach Mode)
Glidepath Mode Active

Glidepath
Indicator
Command Bars
Indicate Descent on
Glidepath

LPV Approach
Active

HSI Set to GPS

Figure 6-15 Glidepath Mode

6-14

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SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Figure 6-16 Glidepath Mode Armed

If vertical guidance becomes or is expected to become
unavailable and the approach downgrades, Glidepath
Mode is disarmed. When vertical guidance becomes
available again, Glidepath Mode is automatically re-armed
under GPS Approach Mode.

Glideslope Mode is available for LOC/ILS approaches
to capture and track the glideslope. Glideslope Mode is
armed when:
• A valid localizer frequency is tuned
• LOC Approach Mode is armed (the APR Key is
pressed and either LOC is the selected navigation
source or a LOC/ILS approach is loaded into the
ﬂight plan; see LOC Approach Mode)

Glideslope Mode (GS)
NOTE: Pressing the CWS Button while Glideslope
Mode is active does not cancel the mode. The
autopilot guides the aircraft back to the glideslope upon release of the CWS Button.

Approach Mode Active

Figure 6-18 Glideslope Mode Armed

Once the localizer has been set as the navigation
source, the localizer and glideslope can be captured. Upon
reaching the glideslope, the ﬂight director transitions to
Glideslope Mode and begins to intercept and track the
glideslope.
Glideslope Mode Active

Active ILS
Frequency
Tuned

Glideslope
Indicator

Command Bars
Indicate Descent on
Localizer/Glideslope Path

HSI Set to LOC2

Figure 6-17 Glideslope Mode
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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-15

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Go Around (GA) Mode
Pushing the GA Switch engages the ﬂight director in a
wings level, 7° 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 pitch and roll active mode ﬁelds. Go Around
Mode disengages the autopilot and arms Altitude Hold
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.
Go Around Mode Active

Autopilot Disconnect
Annunciation Flashes
Yellow 5 sec

Command Bars
Indicate Climb

Figure 6-19 Go Around Mode

6-16

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Roll Modes
• Roll Hold (default mode) — Holds the current
aircraft roll attitude or rolls the wings level,
depending on the commanded bank angle
• Heading Select — Captures and tracks the Selected
Heading
• Navigation (GPS, VOR, LOC) — Captures and
tracks the selected navigation source
• Backcourse — Captures and tracks a localizer
signal for backcourse approaches
• Approach (GPS, VAPP, LOC) — Captures and tracks
the selected navigation source with greater sensitivity
for approach
• Go Around — Commands a constant pitch angle
and wings level while in the air
The following table relates each roll mode to its
respective control and annunciation. Refer to the pitch
modes section for information regarding Go Around and
Takeoff 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.
Roll Hold Mode (ROL)
NOTE: If Roll Hold Mode is activated as a result
of a mode reversion, the ﬂight director rolls the
wings level.

When the ﬂight director is activated (the FD or AP Key
is pressed), 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 6-3.

Roll Mode

Control Annunciation
Roll Hold
(default)
ROL
Heading Select
HDG Key
HDG
Navigation, GPS Arm/Capture/Track
GPS
Navigation, VOR Enroute Arm/Capture/Track
VOR
NAV Key
Navigation, LOC Arm/Capture/Track
LOC
(No Glideslope)
Backcourse Arm/Capture/Track
BC Key
BC
GPS
Approach, GPS Arm/Capture/Track
Approach, VOR Arm/Capture/Track
VAPP
APR Key
Approach, ILS Arm/Capture/Track
LOC
(Glideslope Mode automatically armed)
Go Around (in air)
GA Switch
GA
Table 6-2 Roll Modes

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-17

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Heading Select Mode (HDG)
Figure 6-20 Roll Hold Mode Annunciation

Bank Angle
Flight Director Response
< 6°
Rolls wings level
6° to 22° Maintains current aircraft roll attitude
> 22°
Limits bank to 22°

Heading Select Mode is activated by pressing 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

Table 6-3 Roll Hold Mode Responses

NOTE: Pressing the HDG Knob synchronizes the
Selected Heading to the current heading.

Changing the Roll Reference
The roll reference can be changed by pressing the CWS
Button, establishing the desired bank angle, then releasing
the CWS Button.

Heading Select Mode Active

The Selected Heading is adjusted using the HDG Knob
on either display. Pressing the CWS Button and handﬂying the aircraft does not change the Selected Heading.
The autopilot guides the aircraft back to the Selected
Heading upon release of the CWS Button.
Pitch Hold Mode Active

Command Bars
Track Selected
Heading
Selected
Heading
Selected
Heading
Bug

Figure 6-21 Heading Select Mode
6-18

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SECTION 6 – AUTOMATIC
FLIGHT CONTROL
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 330° at a time result in turn reversals.
Navigation Mode (GPS, VOR, LOC)
NOTE: The selected navigation receiver must have
a valid VOR or LOC signal or active GPS course for
the ﬂight director to enter Navigation Mode.

Pressing the NAV Key selects Navigation Mode.
Navigation Mode acquires and tracks the selected
navigation source on the HSI (GPS, VOR, LOC). The
ﬂight director follows GPS roll steering commands when
GPS is the selected navigation source.
GPS Navigation
Mode Active

When the HSI is coupled to 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.
If the Course Deviation Indicator (CDI) shows greater
than one dot when the NAV Key is pressed, the selected
mode is armed. The armed annunciation appears in white
to the left of the active roll mode. For cases where the
projected course is offset a large distance from the present
course for turn anticipation, GPS Navigation Mode can
be activated with crosstrack error up to 10 nm when the
NAV Key is pressed.

Flight Level
Change Mode
Active

Figure 6-23 GPS Navigation Mode Armed

Altitude Hold
Mode Armed

Command Bars
Indicate Left Turn to
Track GPS Course
and Climb to Intercept Selected Altitude

Selected Course

GPS is Active
Navigation Receiver
on HSI

Figure 6-22 Navigation Mode
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-19

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
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 in anticipation of localizer signal capture 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 is tuned while in VOR Navigation
Mode (VOR Navigation Mode reverts to armed)
• Navigation source is manually switched
• Localizer signal is not captured by the ﬁnal approach
ﬁx (FAF) while in LOC Navigation Mode
Changing the Selected Course
The Selected Course on the PFD is controlled using the
CRS Knob. 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.
Approach Mode (GPS, VAPP, LOC)
NOTE: The selected navigation receiver must have
a valid VOR or LOC signal or active GPS course
for the ﬂight director to enter Approach Mode.

Approach Mode is activated when the APR Key is
pressed. Approach Mode acquires and tracks the selected
navigation receiver on the HSI (GPS, VOR, or LOC),
depending on the loaded approach. This mode uses the
selected navigation receiver deviation and desired course
inputs to ﬂy the approach. Approach Mode provides
greater sensitivity for signal tracking than Navigation
Mode.
Pressing the APR Key when the CDI is greater than
one dot arms the selected approach mode (annunciated
6-20

in white to the left of the active roll mode). If the selected
navigation receiver is GPS, pressing the APR Key arms
GPS Approach Mode, provided that a GPS approach has
been loaded into the ﬂight plan. If the loaded approach
provides WAAS-based vertical guidance, Glidepath Mode
is also armed (Figure 6-16). If GPS Approach Mode is
selected while in GPS Navigation Mode, capture can occur
with crosstrack error of up to 2 nm.
Figure 6-24 GPS Approach Mode Armed

LOC Approach Mode allows the autopilot to ﬂy a LOC/
ILS approach with a glideslope. LOC Approach Mode is
armed (along with Glideslope Mode; see Figure 6-17)
when the APR Key is pressed and either of the following
have been done:
• Navigation source is set to LOC
• A LOC/ILS approach is loaded into the ﬂight plan
and the corresponding localizer frequency tuned
(even if the selected navigation source is GPS)
Localizer capture is suppressed until the navigation
source is changed to LOC.
If Approach Mode is active and either of the following
occur, the ﬂight director reverts to Roll Hold Mode (wings
rolled level):
• Vectors-to-Final is activated
• Navigation source is manually switched
• Localizer signal is not captured by the ﬁnal approach
ﬁx (FAF) while in LOC Navigation Mode
Changing the Selected Course
The Selected Course on the PFD is controlled using the
CRS Knob. 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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Backcourse Mode (BC)

Changing the Selected Course

NOTE: When making a backcourse approach,
set the Selected Course to the localizer front
course.

Backcourse Mode captures and tracks a localizer
signal. The mode may be selected by pressing the BC
Key. Backcourse Mode is armed if the CDI is greater than
one dot when the mode is selected. The ﬂight director
creates roll steering commands from the Selected Course
and deviation when in Backcourse Mode.
Backcourse Mode Active

The Selected Course on the PFD is controlled using the
CRS Knob. Pressing the CWS Button and hand-ﬂying
the aircraft does not reset any reference data while in
Backcourse Mode. The autopilot guides the aircraft back
to the Selected Course (or GPS ﬂight plan) when the CWS
Button is released.

Glideslope Mode Active

LOC2 is Active
Navigation Receiver
on HSI

Figure 6-25 Backcourse Mode

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-21

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

6.4

AUTOPILOT OPERATION
NOTE: Refer to the AFM for speciﬁc instructions
regarding emergency procedures.

Cessna Nav III’s autopilot operates ﬂight control
surface servos to provide automatic ﬂight control. The
autopilot controls the aircraft pitch and roll attitudes
following commands received from the ﬂight director.
Pitch autotrim provides trim commands to the pitch trim
adapter to relieve any sustained effort required by the
pitch servo.

Flight Control
Pitch and roll commands are provided to the servos,
based on the active ﬂight director modes. Servo motor
control limits the maximum servo speed and torque. The
servo gearboxes are equipped with slip-clutches set to
certain values. This allows the servos to be overridden in
case of an emergency.
Pitch Axis and Pitch Trim
The autopilot pitch axis uses pitch rate to stabilize the
aircraft pitch attitude during upsets and ﬂight director
maneuvers. Flight director pitch commands are rate- and
attitude-limited, combined with pitch damper control, and
sent to the pitch servo motor. 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.
When the autopilot is not engaged, the pitch trim servo
may be used to provide manual electric trim. This allows
the aircraft to be trimmed using a control stick switch
rather than the trim wheel. Manual trim commands are
generated with the MET Switch. Trim speeds are scheduled
with airspeed to provide more consistent response.

6-22

Roll Axis
The autopilot roll axis uses roll rate to stabilize aircraft
roll attitude during upsets and ﬂight director maneuvers.
The ﬂight director roll commands are rate- and attitudelimited, combined with roll damper control, and sent to
the roll servo motor.

Engaging the Autopilot
NOTE: Autopilot engagement/disengagement is
not equivalent to servo engagement/disengagement. Use 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.
Autopilot Engaged

Figure 6-26 Autopilot Engaged

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Control Wheel Steering
During autopilot operation, the aircraft may be handﬂown 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 CWS behavior in each mode.
Control Wheel Steering

The autopilot is manually disengaged by pushing the
AP DISC Switch, GA Switch, MET ARM Switch, or the
AP Key on the MFD. Manual disengagement is indicated
by a ﬁve-second ﬂashing yellow ‘AP’ annunciation and a
three-second autopilot disconnect aural alert. After manual disengagement, the autopilot disconnect aural alert
may be cancelled by pushing the MET ARM or AP DISC
Switch (AP DISC Switch also cancels the ﬂashing ‘AP’ annunciation).
Autopilot Manually Disengaged

Figure 6-29 Manual Autopilot Disengagement

Figure 6-27 CWS Annunciation

Disengaging the Autopilot
Automatic disengagement occurs due to:
• System failure
• Inability to compute default ﬂight director modes
(FD also disengages automatically)
• Invalid sensor data
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 MET Switch.
Autopilot Automatically Disengaged

Figure 6-28 Automatic Autopilot Disengagement

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-23

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

6.5

EXAMPLE PROCEDURES
NOTE: The diagrams in this section are for instructional purposes only and should not be used for
navigation.

This section provides a scenario-based set of procedures
showing various GFC 700 AFCS modes used while
following a previously entered ﬂight plan. The following
example closely follows the example ﬂight plan discussed
in the Navigation section. Refer to the example in Section
7 - Navigation when studying the this example.
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 after following
heading vectors of 240˚ and 290˚ assigned by ATC . Airway
V4 is ﬂown to Salina VOR (SLN) using VOR navigation,
then airway V244 is ﬂown using a GPS ﬂight plan. The
ILS approach for runway 35L and LPV (WAAS) approach
for runway 35R are shown and a missed approach is
executed.
33

24
21

30
27

24
21

12
18

KMKC

Lamar
VOR
(LAA)

Salina
VOR
(SLN)

Hays
VOR
(HYS)

V 244

KCOS

Figure 6-30 Flight Plan Overview

6-24

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Departure

c) Press the AP Key to engage the autopilot in a
climb using Vertical Speed Mode.

Climbing to the Selected Altitude and ﬂying
an assigned heading:
1) Use the ALT Knob to set the Selected Altitude to
12,000 feet after takeoff. Depart KMKC:
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) Adjust the aircraft’s vertical speed to the desired
1,000 fpm.
b) Press the VS Key to activate Vertical Speed and
Roll Hold modes and arm Selected Altitude
Capture Mode.
The Vertical Speed Reference may be adjusted
after Vertical Speed Mode is selected using the
NOSE UP/DN Key or pushing the CWS Button
while hand-ﬂying the aircraft to establish a new
Vertical Speed Reference.
HD

3) Press the HDG Key to activate Heading Select Mode
while the autopilot is engaged in the climb.
Use the HDG Knob to set the Selected Heading,
complying with ATC vectors to intercept Airway
V4. The autopilot follows the Selected Heading
Bug on the HSI and turns the aircraft to the desired
heading.

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.

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.

TO M
ode

Selected Altitude of 12,000 MSL
ALT Mode

4
KMKC

Mod

Figure 6-31 Departure
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-25

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Intercepting a VOR Radial

d) Press the NAV Key. This arms VOR Navigation
Mode and the white ‘VOR’ annunciation appears
to the left of the active lateral mode.

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.

2) Once the CDI shows less than one dot, 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.

Intercepting a VOR radial:
1) Arm VOR Navigation Mode:
a) Tune the VOR frequency.
b) Press the CDI Softkey to set the navigation
source to VOR.
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°.

3) The autopilot continues the turn until the aircraft
is established on the Selected Course.

Hd
29 g
0o

255

Salina
VOR
(SLN)

VO
R

NA
V

Mo
de

2
HD

VO
R

21
18

Figure 6-32 Intercepting a VOR Radial

6-26

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SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Flying a Flight Plan/GPS Course

b) Press the NAV Key to activate GPS Navigation
Mode. The autopilot guides the aircraft along
the active ﬂight plan leg.

NOTE: Changing the navigation source cancels
Navigation Mode and causes the ﬂight director
to revert back to Roll Hold Mode (wings rolled
level).

If the NAV Key is not pressed within 10 seconds
of VOR signal loss, the ﬂight director reverts 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.

3) 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.

Flying a GPS ﬂight plan:
1) Enter Salina VOR (SLN) into the GPS ﬂight plan.
2) Transition from VOR to GPS Navigation Mode:
a) Press the CDI Softkey until GPS is the selected
navigation source. Due to VOR signal loss,
VOR Navigation Mode is cancelled. The ‘VOR’
annunciation ﬂashes yellow.
Flashes up to 10 sec, Transitions to Roll Hold
Mode Unless NAV Key is Pressed

NAV

Mod

075

Salina
VOR
(SLN)

V 244

260
o

d
AV Mo
VOR N

076

Hays
VOR
(HYS)

GP S

21
18

Figure 6-33 Transition to GPS Flight Plan
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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-27

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

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 from
12,000 ft:
• 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.
• Non-path descent in a VNV scenario – While
the ﬂight director is following VNV guidance for
descent, 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.

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.

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.

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.

Flight Level Change descent:
1) Select Flight Level Change Mode:
a) Using the ALT Knob, set the Selected Altitude to
10,000 feet.
1
Cruise Altitude of 12,000 MSL
ALT Mode

2
FLC

Mod

3
Selected Altitude of 10,000 MSL
ALT Mode

Figure 6-34 FLC Descent
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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Vertical Path Tracking descent to VNV
Target Altitude:

• Turn the ALT Knob to adjust the Selected
Altitude
• Press the VNV Key

1) Select VNV ﬂight control:
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
at least 75 feet below the ﬂight plan’s VNV
Target Altitude of 10,000 feet.
If the Selected Altitude is not adequately adjusted
below the VNV Target Altitude, the ﬂight director
commands descent to the Selected Altitude rather
than the VNV Target Altitude once Vertical Path
Tracking Mode becomes active (ALTS is armed
rather than ALTV).
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:

ALT Mode

TOD

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.

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.

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.

Cruise Altitude of 12,000 MSL

2
VPT

od e

3
VNAV Target Altitude of 10,000 MSL

BOD

ALT Mode

Selected Altitude (set below VNAV Target Altitude)
Along-track Offset, 3 nm before OPSHN

Figure 6-35 VPTH Descent
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

3 nm

6-29

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Non-path descent using Flight Level
Change Mode:

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.

1) Command a non-path descent using Flight Level
Change Mode:
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.

4) When the next TOD is reached, Vertical Path Tracking
becomes active (may require acknowledgment to
allow descent path capture).
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.

2) Reduce power to allow descent in Flight Level
Change Mode. The autopilot maintains the
Airspeed Reference.

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.
VP

e
Planned
TOD

BOD

ALT Mode

Pla

nn
ed
D

Selected Altitude of 9,400 MSL

VNAV Target Altitude of 10,000 MSL

esc
e

nt
Pa
th

ALT Mode

TOD

VP
TH
M

VNAV Target Altitude of 9,000 MSL

od
e

BOD

ALT Mode

Selected Altitude
3 nm

OPSHN

HABUK

Figure 6-36 Non-path Descent
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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Approach

KCOS

Flying an ILS approach:

PETEY

2
G
HD
e

od
M

PYNON

1
GPS NAV Mode

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.

LOC APR/
GS Mode

1) Transition from GPS Navigation Mode to Heading
Select Mode.
a) Load the Runway 35L ILS approach for KCOS
into the ﬂight plan and select ‘VECTORS’ for the
transition.
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.
d) Use Heading Select Mode to comply with ATC
vectors as requested.

Figure 6-37 ILS Approach to KCOS

c) The navigation source automatically switches to LOC.
After this switch occurs, the localizer signal can be
captured and the autopilot and ﬂight director determine
when to begin the turn to intercept the ﬁnal approach
course.

3) There are two options available at this point, as the
autopilot ﬂies the ILS approach:
• Push the AP DISC Switch at the decision
height and land the aircraft.
• Use the GA Switch to execute a missed
approach.
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6-31

SECTION 6 – AUTOMATIC
FLIGHT CONTROL
Flying a WAAS precision approach:

2) Press the APR Key once clearance for approach has
been acquired. GPS Approach Mode is activated
and Glidepath Mode is armed.

CEGIX

GPS APR/
GP Mode

1) Arm flight director modes for a precision
approach:
a) Make sure the navigation source is set to GPS
(use CDI Softkey to change navigation source).
b) Load the Runway 35R LPV approach for KCOS
into the ﬂight plan.

KCOS

2
FALUR

3) Once the glidepath is captured, Glidepath Mode
becomes active. The ﬂight director now provides
guidance to the Missed Approach Point.

HABUK

PYNON

1
GPS NAV Mode

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.

Figure 6-38 LPV Approach to KCOS

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Go Around/Missed Approach
NOTE: As a result of calculations performed by
the system while ﬂying the holding pattern, the
display may re-size automatically and the aircraft
may not precisely track the holding pattern.

Flying a missed approach:
1) Push the GA Switch at the Decision height and
apply full power to execute a missed approach. The
ﬂight director Command Bars establish a nose-up
climb to follow.
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 and the autopilot disconnect aural
alert.
Flashes 5 sec

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.

MOGAL

2
KCOS

To hold the current airspeed during the climb, press
the FLC Key.

As the aircraft nears the Selected Altitude, the
ﬂight director transitions to Selected Altitude
190-00384-08 Rev. A

GA Mode

3) Use the ALT Knob to set a Selected Altitude to
hold.

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.

GPS NAV Mode

2) Start the climb to the prescribed altitude in the
published Missed Approach Procedure (in this case,
10,000 ft).
a) Press the AP Key to re-engage the autopilot.
b) If navigating an ILS approach, press the CDI
Softkey to select GPS as the navigation source.
c) Press the NAV Key to have the autopilot ﬂy to
the hold.

Capture Mode, indicated by the green ‘ALTS’
annunciation ﬂashing for up to 10 seconds.

Figure 6-39 Go Around/Missed Approach

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

6-33

SECTION 6 – AUTOMATIC
FLIGHT CONTROL

6.6

AFCS ANNUNCIATIONS AND ALERTS

AFCS Status Alerts
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

Figure 6-40 AFCS Status Annunciation

Alert Condition
Aileron Mistrim Right
Aileron Mistrim Left
Elevator Mistrim Down
Elevator Mistrim Up
Pitch Trim Failure
(or stuck MET Switch)

Annunciation

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 MET switches separately to unstick

Roll Failure

Roll axis control failure; AP inoperative

Pitch Failure

Pitch axis control failure; AP inoperative

System Failure

Preﬂight Test

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.
Preﬂight system test failed; aural alert sounds at failure
Table 6-4 AFCS Status Field Alerts

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

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SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Overspeed Protection
Overspeed protection is provided in situations where
the ﬂight director cannot acquire and maintain the vertical
Mode Reference for the selected vertical mode without
exceeding the certiﬁed maximum autopilot airspeed.
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.

Airspeed
Indicator

Figure 6-41 Overspeed Annunciation

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SECTION 6 – AUTOMATIC
FLIGHT CONTROL

Blank Page

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190-00384-08 Rev. A

SECTION 7 – NAVIGATION

SECTION 7: NAVIGATION
The majority of the following discussions pertain to
the Multi Function Display. In discussions pertaining to
the PFD, the controls are located on the PFD.

7.1

NAVIGATION MAP PAGE
WARNING: The map display should only be
used for situational awareness. Any map display
indication should be compared with approved
navigation sources.

7.2

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD
Identiﬁer

Geographic
Region

Facility Name
City

VNAV Target Altitude
Offset Before Selected
Direct-to
Map Orientation

VNAV
Target Altitude
Map of the
Selected
Waypoint

Select the MAP Page Group
1) Turn the large FMS Knob until ‘MAP’ is highlighted
in the page group box in the lower right of the MFD
display.
2) Turn the small FMS Knob to select the ﬁrst MAP
page (indicated by a solid rectangular icon).

Map Range
Bearing
Direct-to
Course

Distance
Activate Field

Figure 7-2 MFD Direct-to Window

Enter a Direct-to Destination
1) Press the Direct-to (

) Key.

2) Enter the destination waypoint identiﬁer.
3) Press the ENT Key to conﬁrm the identiﬁer. The
‘Activate?’ ﬁeld is highlighted.
4) If no altitude constraint or course is desired, press
the ENT Key to activate. To enter an altitude
constraint, proceed to step 5.
5) Turn the large FMS Knob to place the cursor over
the ‘VNAV’ altitude ﬁeld.
6) Enter the desired altitude.
Figure 7-1 Navigation Map Page (Enroute)

7) Press the ENT Key. The option to select ‘MSL’ or
‘AGL’ is now displayed.
8) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

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7-1

SECTION 7 – NAVIGATION
9) Press the ENT Key. The cursor is placed in the ‘VNV’
offset distance ﬁeld.
10) Enter the desired target altitude offset from the
selected Direct-to.
11) Press the ENT Key to highlight ‘Activate?’ or turn the
large FMS Knob to highlight the ‘COURSE’ ﬁeld.
12) Enter the desired course to the waypoint.

Select a Direct-to Destination to a Nearest
Airport
1) Press the Direct-to (

) Key.

2) Turn the small FMS Knob to the left. Initially, a
ﬂight plan waypoint list is displayed as in Figure
7-3. The list is populated only when navigating a
ﬂight plan.

13) Press the ENT Key to highlight ‘ACTIVATE?’.
14) Press the ENT Key again to activate the Direct-to.
Select a Direct-to Destination to a Flight Plan
Waypoint
1) While navigating an active ﬂight plan, press the
Direct-to (
) Key.
2) Turn the small FMS Knob to the left to display a list
of ﬂight plan waypoints as shown in Figure 7-3.

Figure 7-4 Nearest Airport List (MFD)

3) Turn the small FMS Knob to the right to display the
‘NRST’ airports to the aircraft’s current position as
shown in Figure 7-4.
4) Turn the large FMS Knob to select the desired
airport.
5) Press the ENT Key. The cursor is now displayed on
‘ACTIVATE?’.

Figure 7-3 Flight Plan Waypoint List (MFD)

3) Turn the large FMS Knob to select the desired
waypoint.
4) Press the ENT Key. The cursor is now displayed on
‘ACTIVATE?’.
5) Press the ENT Key again to activate a Direct-to.

7-2

6) Press the ENT Key again to activate a Direct-to.
Select a Direct-to Destination to a Recently
Entered Identiﬁer
1) Press the Direct-to (

) Key.

2) Turn the small FMS Knob to the left. Initially, a
ﬂight plan waypoint list is displayed as in Figure
7-3. The list is populated only when navigating a
ﬂight plan.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

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SECTION 7 – NAVIGATION
9) Turn the large FMS Knob to place the cursor in the
‘COURSE’ ﬁeld.
10) Enter the desired course.
11) Press the ENT Key. The cursor now highlights
‘ACTIVATE?’.
Figure 7-5 Recently Entered Waypoints List (MFD)

3) Turn the small FMS Knob to the right to display the
‘RECENT’ waypoints as shown in Figure 7-5.
4) Turn the large FMS Knob to select the desired
airport.
5) Press the ENT Key. The cursor is now displayed on
‘ACTIVATE?’.
6) Press ENT again to activate a Direct-to.
Re-center the CDI to the Destination
Waypoint

12) Press the ENT Key again to begin navigation using
the selected destination, altitude constraint, and
course.
Canceling Direct-to Navigation
1) Press the Direct-to (

) Key.

2) Press the MENU Key to display the Direct-to options
menu.
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.

Press the Direct-to (
) Key, followed by
pressing the ENT Key twice. If a missed approach
point (MAP) is the current destination, the approach
is canceled.

Manually Deﬁne the Active Direct-to
1) Press the Direct-to (

) Key.

2) Turn the large FMS Knob to highlight the ‘VNAV’
altitude ﬁeld.
3) Enter the desired altitude.
4) Press the ENT Key. The option to select ‘MSL’ or
‘AGL’ is now displayed.

Figure 7-6 Canceling Direct-to Navigation

Direct-to Navigation from the PFD
WPT Symbol

WPT Location

Identiﬁer
Facility Name
VNAV Target Altitude
Bearing to WPT
Course to Selected WPT

Offset Distance
Distance from WPT

5) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
6) Press the ENT Key. The cursor now highlights the
VNAV offset ﬁeld.

Figure 7-7 PFD Direct-to Window

7) Enter the desired offset distance.
8) Press the ENT Key.
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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-3

SECTION 7 – NAVIGATION
Enter a Direct-to Destination

Select a Direct-to Destination to a Flight Plan
Waypoint

1) Press the Direct-to Key (
).
2) Turn the large FMS Knob to place the cursor in the
desired selection ﬁeld.

1) While navigating an active ﬂight plan, press the
Direct-to (
) Key.

3) Turn the small FMS Knob to begin selecting the
desired identiﬁer, location, etc.

2) Turn the small FMS Knob to the left to display a list
of ﬂight plan waypoints as shown in Figure 7-8.

4) Press the ENT Key.
5) The cursor is now ﬂashing on ‘ACTIVATE?’. If no
altitude constraint or course is desired, press the
ENT Key to activate. To enter an altitude constraint,
proceed to step 6.
6) Turn the large FMS Knob to place the cursor over
the ‘VNAV’ altitude ﬁeld.
7) Turn the small FMS Knob to enter the desired VNAV
altitude.
8) Press the ENT Key. The option to select ‘MSL’ or
‘AGL’ is now displayed.
9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
10) Press the ENT Key. The cursor is placed in the
‘VNAV’ offset distance ﬁeld.
11) Turn the small FMS Knob to enter the desired target
altitude offset from the selected Direct-to.
12) Press the ENT Key to highlight ‘Activate?’ or turn the
large FMS Knob to highlight the ‘COURSE’ ﬁeld.

Figure 7-8 Flight Plan Waypoint List (PFD)

3) Turn the large FMS Knob to select the desired
waypoint.
4) Press the ENT Key. The cursor is now displayed on
‘ACTIVATE?’.
5) Press the ENT Key again to activate a Direct-to.
Select a Direct-to Destination to a Nearest
Airport
1) Press the Direct-to (

) Key.

2) Turn the small FMS Knob to the left. Initially, a
ﬂight plan waypoint list is displayed as in Figure
7-8. The list is only populated when navigating a
ﬂight plan.

13) Turn the small FMS Knob to enter the desired course
to the waypoint.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT Key again to activate the Direct-to.
Figure 7-9 Nearest Airport List (PFD)

3) Turn the small FMS Knob to the right to display the
‘NRST’ airports to the aircraft’s current position as
shown in Figure 7-9.
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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

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SECTION 7 – NAVIGATION
4) Turn the large FMS Knob to select the desired
airport.
5) Press the ENT Key. The cursor is now displayed on
‘ACTIVATE?’.
6) Press the ENT Key again to activate a Direct-to.
Select a Direct-to Destination to a Recently
Entered Identiﬁer
1) Press the Direct-to (

) Key.

2) Turn the small FMS Knob to the left. Initially, a
ﬂight plan waypoint list is displayed as in Figure
7-8. The list is only populated when navigating a
ﬂight plan.

Figure 7-10 Recently Entered Waypoints List (PFD)

3) Turn the small FMS Knob to the right to display the
‘RECENT’ waypoints as shown in Figure 7-10.
4) Turn the large FMS Knob to select the desired
airport.
5) Press the ENT Key. The cursor is now displayed on
‘ACTIVATE?’.
6) Press the ENT Key again to activate a Direct-to.
Cancelling Direct-to Navigation
1) Press the Direct-to (

) Key.

2) Press the MENU Key to display the Options Window.
The cursor ﬂashes on ‘Cancel Direct-to NAV’.

7.3

NAVIGATING AN EXAMPLE FLIGHT
PLAN
NOTE: The following example ﬂight plan is
for instructional purposes only. All database
information depicted should be considered not
current.

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.
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. Enroute
altitude will be 12,000 feet. An LPV (WAAS) approach
will be selected for runway 35R. A missed approach will
be executed at the Missed Approach Point (MAP). A few
enroute changes are demonstrated.
NOTE: If the loaded arrival procedure has
published altitudes contained in the navigation
database, these are for turbojet aircraft only.
Accept or change these values as desired to meet
the requirements of the clearance.

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
7-11 indicating the active departure leg.
After takeoff, ATC assigns a heading of 240º.

3) Press the ENT Key to cancel the direct-to.

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-5

SECTION 7 – NAVIGATION
2) Figure 7-11 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.

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 7-12.

Figure 7-12 Assigned Heading of 290º
Figure 7-11 Assigned Heading of 240º

7-6

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
4) V4 is now entered into the ﬂight plan.
a) Press the FMS Knob to activate the cursor.
b) The desired entry point for V4 (TOP) must now be
entered. Turn the large FMS Knob to highlight
the desired ﬂight plan insertion point as shown
in Figure 7-13. The V4 entry point (TOP) is placed
immediately above the highlighted waypoint
(SLN).

c) Turn the small FMS Knob to display the Waypoint
Information Window. Enter the desired beginning
point for V4 leg, in this example, Topeka VOR
(TOP) is used as shown in Figure 7-14.

Figure 7-14 Entering V4 Entry Point

d) Press the ENT Key. TOP is now inserted into the
ﬂight plan as in Figure 7-15.
Figure 7-13 Begin Adding V4 to the Flight Plan

Figure 7-15 TOP Inserted into the Flight Plan

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-7

SECTION 7 – NAVIGATION
e) With SLN still highlighted as in Figure 7-15, turn
the small FMS Knob to the right. The Waypoint
Information Page is displayed and the LD AIRWY
Softkey is now available.
f) Press the LD AIRWY Softkey to display the list
of available airways for TOP as seen in Figure
7-16.

Figure 7-17 List of Available Exits for V4

i) If necessary, turn either FMS Knob to select the
desired exit. In this case Salina VOR (SLN) is
selected as seen in Figure 7-17.

Figure 7-16 List of Available Airways for TOP

j) Press the ENT Key. The selected airway and exit
are displayed the prompt “LOAD?” highlighted
as in Figure 7-18.

g) Turn either FMS Knob to highlight V4 in the list
as seen in Figure 7-16.
h) Press the ENT Key. The list of V4 airway exit
points is now displayed as in Figure 7-17.

Figure 7-18 Ready to Load V4

k) Press the ENT Key.
7-8

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
l) V4 is now loaded into the ﬂight plan as shown
in Figure 7-19.

(XTK) distance on the HSI indicating 16.9 nm
to the intercept point. 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.

Figure 7-19 V4 is Loaded in the Flight Plan

5) V4 is now made the active leg of the ﬂight plan.
a) Press the FMS Knob to activate the cursor.
b) Turn the large FMS Knob to highlight SLN. The
TO waypoint of the leg is selected in order to
activate the leg.
c) Press the ACT LEG Softkey. The conﬁrmation
window is now displayed as in Figure 7-20. Note
the TOP to SLN leg is actually part of V4.

Figure 7-21 V4 Now Active Leg
Figure 7-20 Comﬁrm Active Leg

d) Verify the displayed leg is the desired leg and
press the ENT Key. Note in Figure 7-21, the
magenta arrow in the ﬂight plan window and
magenta line on the map indicating V4 is now the
active ﬂight plan leg. Note also, the crosstrack
190-00384-08 Rev. A

6) The aircraft continues on heading 290º. When the
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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-9

SECTION 7 – NAVIGATION
7) As the CDI approaches center, the aircraft turns
onto the active leg as seen in Figure 7-22.

8) At SLN, Victor Airway 244 (V244) is intercepted.
Turn prompts are displayed in the PFD Navigation
Status Box as seen in Figure 7-23.

Figure 7-23 Turn to Intercept V244

9) As seen in Figure 7-24, V244 is now the active ﬂight
plan leg.

Figure 7-22 Turn on to Active Leg

7-10

Figure 7-24 V244 Now Active Leg

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
10) At Lamar VOR (LAA) V263 is intercepted. See Figure
7-25.

Figure 7-26 Direct To OPSHN
Figure 7-25 HYS to LAA Leg Active

d) Turn the large FMS Knob to place the cursor in
the VNV altitude ﬁeld as shown in Figure 7-27.

11) ATC grants clearance to proceed direct to OPSHN
intersection to begin the arrival procedure and
issues a crossing altitude restriction 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
c) Press the Direct-to (
Window is now displayed as shown in Figure
7-26.

Figure 7-27 Enter VNV Altitude

e) An altitude of 10,000 feet is entered as requested
by ATC.

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-11

SECTION 7 – NAVIGATION
f) Press the ENT Key. The cursor is now displayed in
the VNV offset ﬁeld as shown in Figure 7-28.

NOTE: If the loaded arrival procedure has
waypoints with altitude constraints retrieved
from the database, those altitudes are displayed
as white numerals. This indicates the altitudes will
not be used by the system for vertical guidance
until manually accepted by the pilot. To accept
the displayed altitude, place the cursor over the
altitude and press the ENT Key. The altitude entry
then changes to light blue numerals, indicating
the altitude will now be used by the system for
providing vertical guidance.

Figure 7-28 Enter VNV Offset Distance

g) Enter the offset, or distance from the waypoint
at which the selected altitude will be reached. In
this case, three miles prior to OPSHN is entered.
In other words, the G1000 gives vertical guidance
so the aircraft will arrive at an altitude of 10,000
feet three miles prior to OPSHN.
h) Press the ENT Key twice to activate the direct-to.
Note, in Figure 7-29, the magenta arrow in the
Active Flight Plan Window indicating the direct-to
OPSHN after the offset waypoint for OPSHN. The
preceding offset waypoint indicates the offset
distance and altitude that was 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.
7-12

Figure 7-29 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.
a) Press the PROC Key to display the Procedures
Window.
If the GPS system is not WAAS capable, or WAAS
is not available, the LPV approach will not be
displayed in the list of available approaches.
Selecting the LNAV approach for runway 35R gives
vertical guidance up to the IAF.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
b) ‘SELECT APPROACH’ should be highlighted as
shown in Figure 7-30.

d) Turn either FMS Knob to select the LPV approach
for 35R as shown in Figure 7-31.
e) Press the ENT Key. A list of available transitions
for the selected approach is displayed as shown
on Figure 7-32.

Figure 7-30 Procedures Window

c) Press the ENT Key. A list of available approaches
for the destination airport is displayed as in Figure
7-31.

Figure 7-32 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.

Figure 7-31 List of Available Approaches

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-13

SECTION 7 – NAVIGATION
h) With ‘LOAD?’ highlighted, again press the ENT
Key. The selected approach is added to the ﬂight
plan as seen in Figure 7-33.

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 7-34. Vertical
guidance from the FAF to the Missed Approach
Point (MAP) is given using the WAAS GPS altitude
source, therefore, the displayed altitude values
are for reference only.

Figure 7-33 Loaded Approach

13) Note the altitude constraints associated with each
of the approach waypoints as seen in Figure 7-33.
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.
If it is desirable not to 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.

Figure 7-34 Vertical Guidance is Active to the FAF

14) As the aircraft approaches OPSHN, it may be
desirable to adjust how fast, or steep, the upcoming
descent will be. The default Flight Path Angle (FPA)
is -2.5 degrees and a required vertical speed is
computed to maintain the -2.5 FPA. To change the
vertical ﬂight path, perform the following steps.

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.

7-14

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
a) Press the VNV PROF Softkey to place the cursor
in the target vertical speed ﬁeld (VS TGT) as
shown in Figure 7-35.
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.

15) As seen in Figure 7-36, the aircraft is approaching
TOD. Note the target vertical speed required to
reach 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 7-37.

Note the information now displayed in the
‘CURRENT VNV PROFILE’ box. Also, note the
offset waypoint and a gray circle labeled ‘TOD’
are now displayed on the map. The gray circle
marks the Top of Descent (TOD). In this example,
after passing the TOD point, vertical guidance
is provided that results in a -3.0 degree FPA
descent to an altitude of 10,000 feet at the offset
waypoint.

Figure 7-36 Approaching Top of Descent (TOD)

Target
Altitude

Vertical
Deviation
Indicator
(VDI)
Figure 7-35 Adjusting the Descent

c) Press the ENT Key.

Required
Vertical
Speed
Indicator
(RVSI)

Figure 7-37 VDI & RVSI Upon Reaching Top of Descent (TOD)

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-15

SECTION 7 – NAVIGATION
16) Upon reaching TOD, a descent vertical speed is
established which places the VSI pointer in line
with the RVSI as shown in Figure 7-38.

Keep Vertical
Deviation Pointer
Centered

18) The aircraft is approaching OPSHN. The upcoming
turn and next heading is annunciated at the top
left of the PFD as seen in Figure 7-40. 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.

Align Actual
Vertical Speed
with Required
Vertical Speed

Figure 7-38 VDI & RVSI Showing Correctly Established Descent

17) When the aircraft is one minute from the bottom
of descent (BOD) this is annunciated as shown
in Figure 7-39. Upon reaching the OPSHN offset
waypoint (three miles before OPSHN), the aircraft
will be at 10,000 feet.

Figure 7-40 Turn to intercept OPSHN to FSHER Leg

Figure 7-39 Approaching Bottom of Descent (BOD) at OPSHN

7-16

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
19) After passing OPSHN, the next leg of the arrival
turns magenta as shown in Figure 7-41. The
magenta arrow in the ﬂight plan list now indicates
the OPSHN to FSHER leg of the arrival procedure is
now active.

Figure 7-41 Tracking the OPSHN to FSHER Leg

20) The ﬂight continues through the arrival procedure
to PYNON (see Figure 7-42). At a point 31 nautical
miles 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.
There will be a descent to HABUK 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.
Figure 7-42 Approaching PYNON

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-17

SECTION 7 – NAVIGATION
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 7-43).

22) The IAF is the next waypoint. At the TOD, establish
a descent vertical speed as previously discussed in
Step 16. The aircraft altitude will be 9,000 feet
upon reaching HABUK.

Figure 7-43 Approach Leg is Now Active

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 7-44.
Figure 7-45 Descending Turn to the Initial Approach Fix (IAF)

Figure 7-44 Activate Missed Approach

c) Press the ENT Key to activate the approach.
7-18

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
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 7-46) when the ﬁnal
approach course becomes active.

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 7-46.

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 7-47.

Figure 7-47 Descending to the Missed Approach Point
Figure 7-46 Descending to the FAF
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-19

SECTION 7 – NAVIGATION
In this missed approach procedure, the fix
immediately following the MAP (in this case
‘6368FT’) is not part of the published procedure.
It is simply a ﬁx that deﬁnes a leg which guides
the aircraft along the runway centerline until
the required altitude to make the ﬁrst turn on
the missed approach is exceeded. 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 this ﬁx until an altitude
of 6,368 feet reached. After reaching 6,368
feet, a direct-to is established to the published
ﬁx (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. The altitude constraint value defaults
to 400 feet AGL when the ﬁx is not part of the
published procedure.

A direct-to is initiated to MOGAL, which is the
Missed Approach Hold Point (MAHP) as seen in
Figure 7-48. The aircraft is climbing to 10,000
feet. The CDI ﬂight phase now changes from LPV
to MAPR as seen on the HSI.

In some missed approach procedures this altitude
ﬁx may be part of the published procedure. For
example, the procedure dictates a climb to 5,500
feet, then turn left and proceed to the Missed
Approach Hold Point (MAHP). In this case, the
altitude ﬁx would be labeled ‘5500FT’. Again, if
the aircraft altitude is lower than this prescribed
altitude, a direct-to is established to this ﬁx when
the missed approach procedure is activated.

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.
Figure 7-48 Missed Approach Active

7-20

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
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 7-49.

7.4

AIRPORT INFORMATION

Figure 7-51 Airport Information Page
Figure 7-49 Establishing the Holding Pattern

27) The aircraft maintains 10,000 feet while following
the magenta line through the hold as in Figure
7-50.

Select the Airport Information Page
1) Turn the large FMS Knob to select the ‘WPT’ page
group.
2) Turn the small FMS Knob to select the first
rectangular page icon. Initially, information for the
airport closest to the aircraft’s present position is
displayed.
Select an Airport from the Database
1) With the Airport Information Page displayed, press
the FMS Knob to activate the cursor.
2) Enter the desired airport identiﬁer.

Figure 7-50 Hold Established
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-21

SECTION 7 – NAVIGATION
Select an Airport from the Active Flight Plan
1) With the Airport Information Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the small FMS Knob to the left to display a list
of ﬂight plan airports as shown in Figure 7-52.

Figure 7-52 Flight Plan Airport List

3) Turn the large FMS Knob to select the desired
airport.

4) Turn the large FMS Knob to select the desired
airport.
5) Press the ENT Key.
Select a Recently Entered Airport Identiﬁer
1) With the Airport Information Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the small FMS Knob to the left. Initially, a ﬂight
plan waypoint list is displayed as in Figure 7-52.
The list is populated only when navigating a ﬂight
plan.
3) Turn the small FMS Knob to the right to display the
‘RECENT’ airports as shown in Figure 7-54.

4) Press the ENT Key.
Select a Nearest Airport
1) With the Airport Information Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the small FMS Knob to the left. Initially, a
ﬂight plan airport list is displayed as in Figure 7-52.
The list is populated only when navigating a ﬂight
plan.

Figure 7-54 Recently Entered Airports List

4) Turn the large FMS Knob to select the desired
airport.
5) Press the ENT Key.
Select an Airport by Facility Name or City
Location
1) With the Airport Information Page displayed, press
the FMS Knob to activate the cursor.

Figure 7-53 Nearest Airport List

3) Turn the small FMS Knob to the right to display the
‘NRST’ airports to the aircraft’s current position as
shown in Figure 7-53.

2) Turn the large FMS Knob to the right to select the
facility name or location (city) ﬁeld.
3) Enter the desired facility name or city.
5) Press the ENT Key. If there are duplicate names
in the database, a list is displayed from which to
choose the desired location.
6) To remove the flashing cursor, press the FMS
Knob.

7-22

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION
Access Runway Information
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 on the
‘RUNWAYS’ identiﬁer ﬁeld.
3) Turn the small FMS Knob in the direction of the
green arrow to display the next runway for the
selected airport. Continue turning the small FMS
Knob to select the desired runway.

7.5

INTERSECTION INFORMATION

Select the Intersection Information Page
1) Turn the large FMS Knob to select the ‘WPT’ page
group.
2) Turn the small FMS Knob to select the second
rectangular page icon.

4) To remove the flashing cursor, press the FMS
Knob.
Access Frequency Information
1) With the Airport Information Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to move the cursor to the
Frequencies box.
3) Turn either FMS Knob to scroll through the list,
placing the cursor on the desired frequency. If a
listed frequency has sector or altitude restrictions,
the frequency is preceded by an info (‘i’) designation.
Press the ENT Key to view the information. The
following may be displayed with the frequency:
• ‘TX’ – transmit only
• ‘RX’ – receive only
• ‘PT’ – part time frequency
4) Press the ENT Key to place the selected frequency
in the standby ﬁeld of the COM or NAV box.
5) To remove the cursor, press the FMS Knob.

190-00384-08 Rev. A

Figure 7-55 Intersection Information Page

Access Information on an Intersection
1) With the Intersection Information Page displayed,
press the FMS Knob to activate the cursor.
2) Enter an intersection identiﬁer and press the ENT
Key.
3) Press the FMS Knob to remove the flashing
cursor.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-23

SECTION 7 – NAVIGATION

7.6

NDB INFORMATION

Figure 7-56 NDB Information Page

Select the NDB Information Page
1) Turn the large FMS Knob to select the ‘WPT’ page
group.
2) Turn the small FMS Knob to select the third
rectangular page icon
View Information on a Speciﬁc NDB
1) With the NDB Information Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to highlight the desired
selection ﬁeld (identiﬁer, name or closest city).
3) Enter an identiﬁer, name or city and press the ENT
Key.
4) Press the FMS Knob to remove the flashing
cursor.

7.7

VOR INFORMATION

Figure 7-57 VOR Information Page

Select the VOR Information Page
1) Turn the large FMS Knob to select the ‘WPT’ page
group.
2) Turn the small FMS Knob to select the fourth
rectangular page icon.
Access Information on a VOR
1) With the VOR Information Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to highlight the desired
selection ﬁeld (identiﬁer, name or closest city).
3) Enter an identiﬁer, name or city and press the ENT
Key.
4) The ‘FREQUENCY’ ﬁeld is now highlighted. If
desired, press the ENT Key to place the frequency
in the NAV receiver standby ﬁeld.
5) Press the FMS Knob to remove the flashing
cursor.

7-24

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION

7.8

USER WAYPOINT INFORMATION
PAGE

See the Flight Planning section for a discussion on
creating and modifying user deﬁned waypoints.

7.9

NEAREST AIRPORTS

Access Information on a Speciﬁc Airport
1) With the Nearest Airports Page displayed, press the
APT Softkey to place the cursor in the ‘NEAREST
AIRPORTS’ ﬁeld. The ﬁrst airport in the nearest
airports list is highlighted.
2) Turn either FMS Knob to highlight the desired
airport.
3) Press the FMS Knob to remove the flashing
cursor.
Access Runway Information for the Selected
Airport
1) With the Nearest Airports Page displayed, press the
RNWY Softkey to place the cursor in the ‘RUNWAYS’
ﬁeld.
2) Turn the small FMS Knob to select the desired
runway.
3) Press the FMS Knob to remove the flashing
cursor.

Figure 7-58 Nearest Airports Page

Nearest Airport Information on the MFD
Select the Nearest Airports Page

Quickly Tune the COM Transceiver to a
Nearby Airport Frequency
1) With the Nearest Airports Page displayed, press
the FREQ Softkey to place the cursor in the
‘FREQUENCIES’ ﬁeld.

1) Turn the large FMS Knob to select the ‘NRST’ page
group.

2) Turn either FMS Knob to select the desired
frequency.

2) Turn the small FMS Knob to select the first
rectangular page icon.

3) Press the ENT Key. The selected frequency is placed
in the COM standby frequency ﬁeld.

Initially, the closest airport to the aircraft’s present
position is displayed.

4) Press the Frequency Transfer Key to place the
frequency in the active ﬁeld.
5) Press the FMS Knob to remove the flashing
cursor.

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-25

SECTION 7 – NAVIGATION

Nearest Airports Information on the PFD
Bearing TO

7.10 NEAREST INTERSECTIONS

Distance

Airport Symbol
Identiﬁer

Runway Length

Primary COM Frequency

Figure 7-59 Nearest Airports Window

Press the NRST Softkey to display the PFD Nearest Airports Window.
View Information on a Speciﬁc Airport in the
List
1) With the Nearest Airports Window displayed, turn
either FMS Knob to place the cursor on the desired
airport identiﬁer.

Select the Nearest Intersections Page

2) Press the ENT Key to display airport information.

1) Turn the large FMS Knob to select the ‘NRST’ page
group.

3) Press the ENT Key again (cursor is on ‘BACK’) to
return to the list.

2) Turn the small FMS Knob to select the second
rectangular page icon.

Load an Airport COM Frequency into the
Active COM
1) With the Nearest Airports Window displayed, turn
either FMS Knob to place the cursor on the desired
airport frequency shown in the window.
2) Press the ENT Key and the selected frequency is
placed in the COM standby frequency ﬁeld.
3) Press the Frequency Transfer Key to make the
frequency the active frequency.

7-26

Figure 7-60 Nearest Intersections Page

View Information on the Nearest Intersection
1) With the Nearest Intersections Page displayed, press
the FMS Knob to activate the cursor.
2) Turn either FMS Knob to select the desired
intersection.
3) Press the FMS Knob to remove the flashing
cursor.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 7 – NAVIGATION

7.11 NEAREST NDB

7.12 NEAREST VOR

Figure 7-62 Nearest VOR Page

Figure 7-61 Nearest NDB Page

Select the Nearest NDB Page
1) Turn the large FMS Knob to select the ‘NRST’ page
group.
2) Turn the small FMS Knob to select the third
rectangular page icon.
Access Information on a Speciﬁc NDB
1) With the Nearest NDB Page displayed, press the
FMS Knob to activate the cursor.
2) Turn either FMS Knob to select the desired NDB.
The remaining information on the Nearest NDB
Page pertains to the selected NDB.
3) Press the FMS Knob to remove the flashing
cursor.

Select the Nearest VOR Page
1) Turn the large FMS Knob to select the ‘NRST’ page
group.
2) Turn the small FMS Knob to select the fourth
rectangular page icon.
View Information on the Nearest VOR
1) With the Nearest VOR Page displayed, press the
VOR Softkey to place the cursor in the ‘NEAREST
VOR’ box.
2)

Turn either FMS Knob to select a VOR.

3) Press the FMS Knob to remove the flashing
cursor.
Select and Load a VOR Frequency
1) With the Nearest VOR Page displayed, press the
FREQ Softkey to highlight the VOR frequency in the
‘FREQUENCY’ ﬁeld.

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

7-27

SECTION 7 – NAVIGATION
2) Press the ENT Key. The selected VOR frequency is
placed in the NAV standby frequency ﬁeld.

Waypoint Page pertains to the selected Nearest
User Waypoint.

3) Press the FMS Knob to remove the flashing
cursor.

7.13 NEAREST USER WAYPOINT

Figure 7-63 Nearest User Waypoints Page

Select the Nearest User Waypoint Page
1) Turn the large FMS Knob to select the ‘NRST’ page
group.
2) Turn the small FMS Knob to select the fifth
rectangular page icon.
Select a Nearest User Waypoint
1) With the Nearest User Waypoint Page displayed,
press the FMS Knob to activate the cursor. If
any previously entered User Waypoints are within
200 nm, they are displayed with the closest listed
ﬁrst.
2) Turn either FMS Knob to select the desired waypoint.
The remaining information on the Nearest User
7-28

7.14 NEAREST FREQUENCIES

Figure 7-64 Nearest Frequencies Page

Select the Nearest Frequencies Page
1) Turn the large FMS Knob to select the ‘NRST’ page
group.
2) Turn the small FMS Knob to select the sixth
rectangular page icon.
Select and Load the Nearest ARTCC, FSS, or
Weather Frequency
1) With the Nearest Frequencies Page displayed, press
the ARTCC, FSS, or WX Softkey to place the cursor
in the appropriate ﬁeld.
2) Turn the FMS Knobs to select the desired facility or
frequency.

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SECTION 7 – NAVIGATION
3) Press the ENT Key to load the frequency into the
COM frequency standby ﬁeld.

• If the aircraft has entered an airspace, ‘Inside’ is
displayed.

4) Press the FMS Knob to remove the flashing
cursor.

View Additional Details for a Listed Airspace

7.15 NEAREST AIRSPACES

1) With the Nearest Airspace Page displayed, press
the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to scroll through the list,
highlighting the desired airspace.
3) Press the ALERTS Softkey to place the cursor in the
‘AIRSPACE ALERTS’ ﬁeld.
4) Turn either FMS Knob to select the desired
airspace.
5) Press the FMS Knob to remove the flashing
cursor.
View and Quickly Load the Frequency for a
Controlling Agency

Figure 7-65 Nearest Airspaces Page

Select the Nearest Airspaces Page
1) Turn the large FMS Knob to select the ‘NRST’ page
group.
2) Turn the small FMS Knob to select the seventh
rectangular page icon.

1) With the Nearest Airspace Page displayed, press the
FREQ Softkey to place the cursor in ‘FREQUENCIES’
ﬁeld.
2) Turn either FMS Knob to select the desired
frequency.
3) Press the ENT Key to load the frequency into the
COM frequency standby ﬁeld.
4) Press the FMS Knob to remove the flashing
cursor.

Airspace Alerts Box
• If the projected course takes the aircraft inside an
airspace within the next ten minutes, ‘Ahead’ is
displayed.
• If the aircraft is within two nautical miles of an
airspace and the current course takes the aircraft
inside, ‘Ahead < 2 nm’ is displayed.
• If the aircraft is within two nautical miles of an
airspace and the current course will not take the
aircraft inside, ‘Within 2 nm’ is displayed.
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SECTION 7 – NAVIGATION

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SECTION 8 – FLIGHT PLANNING

SECTION 8: FLIGHT PLANNING
The following discussions pertain to the Multi Function
Display, unless otherwise indicated.

8.1

USER DEFINED WAYPOINTS

4) Repeat steps 2 and 3 until the desired name is
entered.
5) Press the ENT Key.
6) Press the ENT Key again to accept the new waypoint
identiﬁer.
7) The cursor is now in the ‘REFERENCE WAYPOINTS’
ﬁeld. If desired, the waypoint can be deﬁned by a
reference waypoint. Turn the FMS Knobs to enter
the position coordinates or the radial and distance
from the reference waypoint.
8) Press the FMS Knob to remove the flashing
cursor.
Modify a User Waypoint
1) With the User Waypoint Information Page displayed,
press the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to move the cursor to the
desired ﬁeld and turn the small FMS Knob to make
changes.

Figure 8-1 User WPT Information Page

Select the User WPT Information Page
1) Turn the large FMS Knob to select the ‘WPT’ page
group.
2) Turn the small FMS Knob to select the fifth
rectangular page icon.
Create a New User Waypoint
1) With the User Waypoint Information Page displayed,
press the NEW Softkey. A waypoint is created at
the current aircraft position.
2) Turn the small FMS Knob to enter ﬁrst character of
the waypoint name.

3) Press the ENT Key to accept the changes.
4) Press the FMS Knob to remove the flashing
cursor.
Delete a User Waypoint
1) Select the User Waypoint Information Page and
press the MENU Key to display the User Waypoint
Information Page Options or press the DELETE
Softkey.
2) Turn the large FMS Knob to select ‘Delete User
Waypoint’ and press the ENT Key. The message
‘Would you like to delete the user waypoint’ is
displayed. With ‘YES’ highlighted, press the ENT
Key.

3) Turn the large FMS Knob to move the cursor to the
next character ﬁeld.
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8-1

SECTION 8 – FLIGHT PLANNING

Create User Waypoints from the Navigation
Map Page
1) With the Navigation Map Page displayed, push
the Joystick to activate the panning function. The
target pointer is displayed at the present aircraft
position.
2) Move the Joystick to place the pointer at the
desired position
3) Press the ENT Key. The User Waypoint Information
Page is now displayed with the captured position.
If the pointer is inside an airspace, a dialog box will
appear giving the choice to review the airspace
information, or create a waypoint.
4) Turn the FMS Knobs to select a waypoint name.
5) Press the ENT Key to accept the selected name. The
ﬁrst reference waypoint ﬁeld is highlighted.

Figure 8-3 Active Flight Plan Page on the MFD

8.3

ACTIVATE A STORED FLIGHT PLAN

1) Press the FPL Key and turn the small FMS Knob to
display the Flight Plan Catalog Page.

6) If desired, turn the FMS Knobs to enter the identiﬁer
of the reference waypoint and the radial and
distance to the reference waypoint. Press the ENT
Key to accept.
7) Press the FMS Knob to remove the ﬂashing cursor or
press the GO BACK Softkey to return to the map.

8.2

VIEWING THE ACTIVE FLIGHT PLAN
Press the FPL Key.

Figure 8-4 Flight Plan Catalog Page

2) Press the FMS Knob to activate the cursor.
Figure 8-2 Active Flight Plan Window on the PFD

3) Turn the large FMS Knob to highlight the desired
ﬂight plan and press the ACTIVE Softkey.
4) With ‘OK’ highlighted, press the ENT Key to activate
the ﬂight plan. To cancel the ﬂight plan activation,
turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.

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SECTION 8 – FLIGHT PLANNING

8.4

ACTIVATE A FLIGHT PLAN LEG

1) From the Active Flight Plan Page, press the FMS
Knob to activate the cursor and turn the large
FMS Knob to highlight the desired destination
waypoint.
2) Press the ACT LEG Softkey (using MFD only).
Or:
Press the MENU Key, select the ‘Activate Leg’ option
from the page menu and press the ENT Key. This
step must be used when activating a leg from
the PFD.

3) With ‘Activate’ highlighted, press the ENT Key.

Figure 8-7 Delete Flight Plan Conﬁrmation

8.6

INVERT ACTIVE FLIGHT PLAN

1) From the Active Flight Plan Page, press the MENU
Key to display the Page Menu.
2) Turn the large FMS Knob to highlight ‘Invert Flight
Plan’ and press the ENT Key. The original ﬂight
plan remains intact in its ﬂight plan catalog storage
location.
3) With ‘OK’ highlighted, press the ENT Key to invert
the ﬂight plan.

Figure 8-5 Activate Flight Plan Leg Conﬁrmation

8.5

STOP NAVIGATING A FLIGHT PLAN

1) Press the FPL Key to display the Active Flight Plan
Page.
2) Press the MENU Key to display the Page Menu
window.

Figure 8-8 Invert Flight Plan

Figure 8-9 Invert Flight Plan Conﬁrmation

Figure 8-6 Delete Flight Plan

3) Turn the large FMS Knob to highlight ‘Delete Flight
Plan’ and press the ENT Key. With ‘OK’ highlighted,
press the ENT Key to deactivate the ﬂight plan. This
will not delete the stored ﬂight plan, only the active
ﬂight plan.
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8-3

SECTION 8 – FLIGHT PLANNING

8.7

CREATE A NEW FLIGHT PLAN

Create a New Flight Plan Using the MFD
1) Press the FPL Key and turn the small FMS Knob to
display the Flight Plan Catalog Page.
2) Press the NEW Softkey to display a blank ﬂight plan
page for the ﬁrst empty storage location.

Create a New Flight Plan Using the PFD
NOTE: A ﬂight plan cannot be entered using the
PFD if another ﬂight plan is active.
NOTE: After the ﬁrst leg is entered (using the
PFD only), it is immediately activated.

1) Press the FPL Key, then press the FMS Knob to
activate the cursor.

Figure 8-10 Create FPL on MFD

3) Turn the small FMS Knob to display the Waypoint
Information Window.
4) Turn the small FMS Knob to the right enter the
ﬁrst character of the identiﬁer of the departure
waypoint. Turning the knob to the left accesses
the FPL, NRST, and RECENT waypoint list.
5) Turn the large FMS Knob to move the cursor to the
next character ﬁeld. Repeat steps 4 and 5 until the
desired identiﬁer has been entered.

Figure 8-11 Waypoint Info Window

2) Turn the small FMS Knob to enter the ﬁrst letter of
the destination waypoint identiﬁer. Turn the large
FMS Knob to the right to move the cursor to the
next character position.
3) Repeat step 2 to spell out the rest of the waypoint
identiﬁer.
4) Press the ENT Key and the cursor is now ready for
entering of the next ﬂight plan waypoint.
5) Repeat steps 2 through 4 to enter the identiﬁer for
each additional ﬂight plan waypoint.
6) Once all waypoints have been entered, press the
FMS Knob remove the cursor. The new ﬂight plan
is now active.

Figure 8-12 Creating Flight Plan on the PFD

6) Press the ENT Key.
7) Repeat step number 3, 4, and 5 to enter the
identiﬁer for each additional ﬂight plan waypoint.
8) 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.
8-4

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SECTION 8 – FLIGHT PLANNING

8.8

ENTER AN AIRWAY IN A FLIGHT
PLAN

5) When the desired entry point is entered, press the
ENT Key.

1) Press the FPL Key to display the active ﬂight plan
or display a stored ﬂight plan.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the waypoint
before which the airway is to be entered.
Figure 8-15 Airway Entry Point Loaded

6) Turn the small FMS Knob to display the Waypoint
Information Window and begin entering the desired
airway identiﬁer.

Figure 8-13 Airway Insertion Point

4) Turn the small FMS Knob to display the Waypoint
Information Window and begin entering the desired
airways entry point.

Figure 8-16 Enter Airway Identiﬁer

7) When the desired airway is entered, press the LD
AIRWY Softkey.

Figure 8-14 Load Airway Entry Point

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8-5

SECTION 8 – FLIGHT PLANNING
8) Turn either FMS Knob to scroll through the list of
available exit points.

8.11 LOAD AN APPROACH
See the Procedures section for a discussion on loading
and activating approach procedures.

8.12 REMOVE A DEPARTURE, ARRIVAL,
APPROACH, OR AIRWAY FROM A
FLIGHT PLAN
1) With the Active or Stored Flight Plan Page displayed,
press the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to highlight the title for
the approach, departure, arrival, or airway to be
deleted. Titles appear in white directly above the
procedure’s waypoints.
Figure 8-17 Select Desired Exit Point

9) With the desired exit point highlighted, press the
ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.

3) Press the CLR Key to display a conﬁrmation window.
With ‘OK’ highlighted, press the ENT Key to remove
the selected procedure or airway.

8.13 STORE A FLIGHT PLAN
1) After creating a ﬂight plan on either the PFD or
MFD, it may be saved by pressing the MENU Key.
2) Turn the large FMS Knob to highlight ‘Store Flight
Plan’ and press the ENT Key.
3) With ‘OK’ highlighted, press the ENT Key to store
the ﬂight plan.

Figure 8-18 Airway Added to Flight Plan

8.9

LOAD A DEPARTURE

Figure 8-19 Store Flight Plan Conﬁrmation

See the Procedures section for a discussion on loading
and activating departure procedures.

8.10 LOAD AN ARRIVAL
See the Procedures section for a discussion on loading
and activating arrival procedures.
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SECTION 8 – FLIGHT PLANNING

8.14 EDIT A STORED FLIGHT PLAN
1) Press the FPL Key and turn the small FMS Knob to
display the Flight Plan Catalog Page.

8.16 INVERT AND ACTIVATE A STORED
FLIGHT PLAN

2) Press the FMS Knob to activate the cursor.

1) From the Flight Plan Catalog Page, press the FMS
Knob to activate the cursor.

3) Turn the large FMS Knob to highlight the desired
ﬂight plan and press the ENT Key.

2) Turn the large FMS Knob to highlight the desired
ﬂight plan.

4) Turn the large FMS Knob to place the cursor in the
desired locations for entering changes.

3) Press the INVERT Softkey. ‘Invert and activate
stored ﬂight plan?’ is displayed.

5) Turn the FMS Knobs to make the desired changes,
then press the ENT Key.

4) With ‘OK’ highlighted, press the ENT Key. The
selected ﬂight plan is now inverted and activated.
The original ﬂight plan remains intact in its ﬂight
plan catalog storage location.

6) Press the FMS Knob to return to the Flight Plan
Catalog Page.

8.15 DELETE A WAYPOINT FROM THE
FLIGHT PLAN
1) With either the Active or Stored Flight Plan
displayed, press the FMS Knob to activate the
cursor.
2) Turn the large FMS Knob to select the waypoint to
be deleted.
3) Press the CLR Key to display a ‘REMOVE (Wpt
Name)’ conﬁrmation window.

8.17 COPY A FLIGHT PLAN
1) From the Flight Plan Catalog press the FMS Knob
to activate the cursor
2) Turn the large FMS Knob to highlight the ﬂight plan
to be copied.
3) Press the COPY Softkey.
4) A ‘Copy to ﬂight plan #?’ conﬁrmation window is
displayed. With ‘OK’ highlighted, press the ENT Key
to copy the ﬂight plan. To cancel, turn the large
FMS Knob to highlight ‘CANCEL’ and press the ENT
Key.

Figure 8-20 Remove Waypoint Conﬁrmation

4) With ‘OK’ highlighted, press the ENT Key to remove
the waypoint. To cancel the delete request, turn the
large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
5) Once all changes have been made, press the FMS
Knob to remove the cursor.

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8-7

SECTION 8 – FLIGHT PLANNING

8.18 DELETE A FLIGHT PLAN

8.20 TRIP PLANNING

1) From the Flight Plan Catalog Page, press the FMS
Knob to activate the cursor.

1) Turn the large FMS Knob to select the ‘AUX’ page
group.

2) Turn the large FMS Knob to highlight the ﬂight plan
to be deleted.

2) Turn the small FMS Knob to select the first
rectangular page icon.

3) Press the DELETE Softkey.

3) The current page mode is displayed at the top of the
page: ‘AUTOMATIC’ or ‘MANUAL’. To change the
page mode, press the AUTO or MANUAL Softkey.

4) A ‘Delete ﬂight plan #?’ conﬁrmation window is
displayed. With ‘OK’ highlighted, press the ENT
Key to delete the ﬂight plan. To cancel, turn the
large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.

Starting WPT

Ending WPT

8.19 GRAPHICAL FLIGHT PLAN CREATION
1) Press the FPL Key to display the Active Flight Plan
Page.
2) Press the Joystick to activate the map pointer. Use
the Joystick to move the pointer to the desired
point on the map to be inserted as a waypoint in
the ﬂight plan.
3) Press the LD WPT Softkey. The selected waypoint is
inserted at the end of the ﬂight plan. The default
user waypoint naming is USR000, USR001, USR002
and so on.
4) If the selected waypoint is to be placed elsewhere in
the ﬂight plan, press the FMS Knob to activate the
cursor. Waypoints are inserted ABOVE the cursor.
5) After placing the cursor at the desired point in the
list of waypoints, press the LD WPT Softkey.
6) To change the user waypoint name, follow the
procedure for modifying a user waypoint.

Figure 8-21 Trip Planning Page

4) For Direct-to planning, press the WPTS Softkey and
verify that the starting waypoint ﬁeld indicates
‘P.POS’ (present position). If necessary, press the
MENU Key and select ‘Set WPT to Present Position’
to display ‘P.POS’. Press the ENT Key and the
ﬂashing cursor moves to the ending waypoint ﬁeld.
Turn the FMS Knobs to enter the identiﬁer of the
ending waypoint and press the ENT Key to accept
the waypoint.
Or:

8-8

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SECTION 8 – FLIGHT PLANNING
For point-to-point planning, turn the FMS Knobs to
enter the identiﬁer of the starting waypoint. Once
the waypoints identiﬁer is entered, press the ENT
Key to accept the waypoint. The ﬂashing cursor
moves to the ending waypoint. Again, turn the FMS
Knobs to enter the identiﬁer of the ending waypoint
and press the ENT Key to accept the waypoint.
Or:
For ﬂight plan leg planning, press the FPL Softkey (at
the bottom of the display) and turn the small FMS
Knob to select the desired ﬂight plan (already stored
in memory), by number. Turn the large FMS Knob
to highlight the ‘LEG’ ﬁeld and turn the small FMS
Knob to select the desired leg of the ﬂight plan, or
select ‘CUM’ to apply trip planning calculations to
the entire ﬂight plan. Selecting ‘FPL 00’ displays the
active ﬂight plan. If the active ﬂight plan is selected,
‘REM’ is an available option to display planning
data for the remainder of the ﬂight plan.
NOTE: The Page Mode must be set to MANUAL
to perform the following steps.

5) Turn the large FMS Knob to highlight the departure
time (DEP TIME) ﬁeld.

7) Turn the FMS Knobs to enter the fuel ﬂow. Press
the ENT Key when ﬁnished. Note that in automatic
page mode, fuel ﬂow is provided by the system.
8) The ﬂashing cursor moves to the fuel on board ﬁeld.
Turn the FMS Knobs to modify the fuel on board.
Press the ENT Key when ﬁnished. In ‘AUTOMATIC’
mode, fuel onboard is provided by the entry made
in ‘GAL REM’ on the EIS System Page.
9) The ﬂashing cursor moves to the calibrated airspeed
ﬁeld. Turn the FMS Knobs to enter a calibrated
airspeed. Press the ENT Key when ﬁnished.
10) The ﬂashing cursor moves to the indicated altitude
field. Turn the FMS Knobs to enter indicated
altitude. Press the ENT Key when ﬁnished.
11) The flashing cursor moves to the barometric
pressure ﬁeld. Turn the FMS Knobs to enter the
altimeter barometric pressure setting. Press the
ENT Key when ﬁnished.
12) The flashing cursor moves to the total air
temperature ﬁeld. Turn the FMS Knobs to enter
the total air temperature. Press the ENT Key when
ﬁnished.

NOTE: The departure time on the Trip Planning
Page is used for preﬂight planning. Refer to the
Utility Page for the actual ﬂight departure time.

6) Turn the FMS Knobs to enter the departure time.
Press the ENT Key when ﬁnished. (Departure time
may be entered in local or UTC time, depending
upon system settings).

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8-9

SECTION 8 – FLIGHT PLANNING

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SECTION 9 – PROCEDURES

SECTION 9: PROCEDURES
9.1

ARRIVALS AND DEPARTURES

Load and Activate a Departure Procedure
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT
DEPARTURE’.
3) Press the ENT Key.
4) If a ﬂight plan is active, the departure airport
is displayed as the default. A list of available
departures is also displayed. If no ﬂight plan is
active, use the FMS Knobs to enter the identiﬁer
of the desired airport. Press the ENT Key.
5) Turn the large FMS Knob to highlight the Departure
ﬁeld. Turn the small FMS Knob to display a list of
available departures.
6) Turn either FMS Knob to select the desired departure
and press the ENT Key.

Figure 9-2 Select Departure Transition

9) With ‘LOAD?’ highlighted, press the ENT Key. The
departure is active when the ﬂight plan is active.

Load and Activate An Arrival Procedure
NOTE: If any portion of an arrival procedure is
the active leg of a ﬂight plan, the existing arrival
procedure must be deleted before changing to a
different arrival procedure.

1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT
ARRIVAL’.
3) Press the ENT Key.
4) If a ﬂight plan is active, the destination airport is
displayed as the default. A list of available arrivals
is also displayed. If no ﬂight plan is active, use the
FMS Knobs to enter the identiﬁer of the desired
airport. Press the ENT Key.

Figure 9-1 Select Departure

7) A list of runways may be displayed for the departure.
Turn either FMS Knob to select the desired runway
and press the ENT Key.

5) Turn the large FMS Knob to highlight the Arrival
ﬁeld. Turn the small FMS Knob to display a list of
available arrivals.
6) Turn either FMS Knob to select the desired arrival
and press the ENT Key.

8) A list of available transitions is displayed for the
departure. Turn either FMS Knob to highlight the
desired transition waypoint and press the ENT
Key.

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9-1

SECTION 9 – PROCEDURES

9.2

APPROACHES
NOTE: If certain GPS parameters (WAAS, RAIM,
etc.) are not available, some published approach
procedures for the desired airport may not be
displayed in the list of available approaches.

Figure 9-3 Select Arrival

7) A second window is displayed listing available
transitions for the arrival. Turn either FMS Knob to
highlight the desired transition waypoint and press
the ENT Key.

Figure 9-4 Select Arrival Transition

8) A third window is displayed listing the available
runways. Turn either FMS Knob to select the desired
runway and press the ENT Key.

Not all approaches in the database are approved for GPS
use. 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.
The G1000 GPS allows for ﬂying LNAV, LNAV/VNAV
(WAAS only), and LPV (WAAS only) approaches according to the published chart. The active appoach type is
annunciated on the HSI as shown in the following table:
HSI
ANNUNCIATION

LNAV
LNAV+V*
Figure 9-5 Select Arrival Runway

9) With ‘LOAD?’ highlighted, press the ENT Key. If a
ﬂight plan is active, the selected arrival procedure is
inserted after the destination airport and becomes
part of the active ﬂight plan. If no ﬂight plan is active
when the arrival is loaded, the arrival procedure
becomes the active ﬂight plan.
9-2

L/VNAV*
LPV*

DESCRIPTION

GPS approach using published
LNAV minima.
GPS approach using published
LNAV minima. Advisory vertical
guidance is provided.
GPS approach using published
LNAV/VNAV minima.
GPS approach using published
LPV minima.

* WAAS systems only

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SECTION 9 – PROCEDURES

Load and/or Activate an Approach Procedure
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT
APPROACH’.
3) Press the ENT Key.
4) If a ﬂight plan is active, the destination airport
is displayed as the default. A list of available
approaches is also displayed. If no ﬂight plan is
active, use the FMS Knobs to enter the identiﬁer of
the desired airport. Press the ENT Key.

7) The cursor moves to the TRANSITIONS ﬁeld. Turn
the large FMS Knob to highlight the desired
transition waypoint and press the ENT Key. (The
“Vectors” option assumes vectors will be received
to the ﬁnal course segment of the approach and
will provide navigation guidance relative to the ﬁnal
approach course.)

5) Turn the large FMS Knob to highlight the Approach
ﬁeld. Turn the small FMS Knob to display a list of
available approaches.

Figure 9-7 Selecting an Approach Transition

Figure 9-6 Selecting an Approach Procedure

6) Turn either FMS Knob to highlight the desired
approach. Press the ENT Key.

8) Turn the large FMS Knob to highlight ‘Activate?’
and press the ENT Key to activate the approach.
Activating the approach initiates a direct-to for
IAF and the G1000 immediately begins navigating
to the IAF. Selecting ‘Load?’ adds the procedure
to the ﬂight plan without immediately using it for
navigation guidance.

Activate An Approach in the Active Flight Plan
1) With the Navigation Map Page displayed, press the
PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE
APPROACH’.
3) Press the ENT Key. The approach procedure is now
active and a direct-to is initiated to the IAF.

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SECTION 9 – PROCEDURES

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SECTION 10 – HAZARD
AVOIDANCE

SECTION 10: HAZARD AVOIDANCE
10.1 CUSTOMIZING THE HAZARD
DISPLAYS ON THE NAVIGATION MAP
1) With the Navigation Map Page displayed, press
the MENU Key to display the Navigation Map
Page Menu. The cursor ﬂashes on the ‘Map Setup’
option.
2) Press the ENT Key. The Map Setup Menu is
displayed. Turn the small FMS Knob to select the
‘Weather’ group (Figure 10-2) to customize the
display of weather features. Select ‘Trafﬁc’ to
customize the display of trafﬁc.
3) Press the small FMS Knob to return to the
Navigation Map Page.

10.2 STORMSCOPE® (OPTIONAL)
WARNING: The Stormscope system is not
intended to be used for hazardous thunderstorm
penetration. Weather information on the G1000
MFD is approved for weather avoidance only.
Refer to the WX-500 Pilot’s Guide for detailed
operation.

Displaying Stormscope Lightning Data on the
Navigation Map Page
1) Press the MAP Softkey.
2) Press the STRMSCP Softkey. Press the STRMSCP
Softkey again to remove Stormscope Lightning Data
from the Navigation Map Page.

Figure 10-1 Page Menu

Figure 10-2 Map Setup Menu

Figure 10-4 In-Flight Navigation Map Page Displaying
Stormscope Lightning Data

Lightning Age
Strike is less than 6 seconds old

Symbol

Strike is between 6 and 60 seconds old
Figure 10-3 Map Setup Group List
190-00384-08 Rev. A

Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old

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10-1

SECTION 10 – HAZARD
AVOIDANCE
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.

Stormscope Page
1) Turn the large FMS Knob until the Map Page group
is selected.
2) Turn the small FMS Knob until the Stormscope
Page is selected. This is the third rectangular page
icon.

Figure 10-5 Lightning Display Range Annunciation

Select ‘cell’ or ‘strike’ as the Stormscope
lightning mode:
1) With the Weather Group selected, press the ENT
Key. The cursor ﬂashes on ‘STRMSCP LTNG’.
2) Turn the large FMS Knob to select ‘STRMSCP
MODE’.
3) Turn the small FMS Knob to display the ‘Cell/Strike’
window.
4) Turn either FMS Knob to select ‘Cell’ or ‘Strike’.
Press the ENT Key.
5) Push the FMS Knob to return to the Navigation
Map Page.
Clear Stormscope lightning data from the
Navigation Map Page:
1) Press the MENU Key (with the Navigation Map Page
displayed).
2) Turn either FMS Knob to highlight the ‘Clear
Stormscope® Lightning’ ﬁeld and press the ENT
Key.

NOTE: If heading input is lost, strikes and/or cells
must be cleared manually after the execution of
each turn. This is to ensure that the strike and/or
cell positions are depicted accurately in relation
to the nose of the aircraft.
10-2

Figure 10-6 Stormscope Page

Change the Stormscope lightning mode
between ‘cell’ and ‘strike’:
1) Select the Stormscope Page.
2) Press the MODE Softkey. The CELL and STRIKE
Softkeys are displayed. 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 located in the upper left corner of
the Stormscope Page.
NOTE: “Cell mode” uses a clustering program to
identify clusters of electrical activity that indicate
cells.

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190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE
Change the viewing mode between 360˚ and
120˚:
1) Select the Stormscope Page.
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.
Press the CLEAR Softkey to remove all Stormscope
lightning data from the display.

10.3 XM WEATHER (SERVICE OPTIONAL)
WARNING: XM Weather is not intended to
be used for hazardous weather penetration.
Weather information provided by XM Radio
Service is approved only for weather avoidance,
not penetration.

NOTE: Weather is not displayed on the Navigation
Map Page at zoom levels less than 10 nm.

Displaying METAR and TAF information on the
Airport Information Page
1) Turn the large FMS Knob to select the WPT Page
Group.
2) Turn the small FMS Knob to select the Airport
Information Page.
3) Press the WX Softkey to display METAR and TAF
text (METAR and TAF information is updated every
12 minutes).

1) From the Navigation Map Page, press the MAP
Softkey.
2) Press the NEXRAD or XM LTNG Softkey to display
the desired weather. Press the applicable softkey
again to remove weather data from the Navigation
Map Page.

METAR
Text

TAF
Text

WX
Softkey
Figure 10-8 METAR and TAF Text Displayed on the
Airport (Weather) Information Page

Figure 10-7 Navigation Map Page Displaying NEXRAD Weather
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-3

SECTION 10 – HAZARD
AVOIDANCE

Displaying Weather on the Weather Data Link
Page
Select 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 fourth
rectangular page icon.
3) Press the available softkeys to select the desired
XM weather product.
4) Press the LEGEND Softkey to view the legends for
the selected products. If necessary, turn either FMS
Knob to scroll through the list. Press the small FMS
Knob or the ENT Key to return to the map.

NEXRAD Limitations
Certain limitations exist regarding the NEXRAD radar
displays. Some, but not all, are listed here:
• NEXRAD base reflectivity does not provide
sufﬁcient information to determine cloud layers or
precipitation characteristics (hail vs. rain, etc).
• An individual NEXRAD site cannot depict high
altitude storms at close ranges, and has no
information about storms directly over the site.
• The resolution of displayed NEXRAD data is 4 square
kilometers. Therefore, when zoomed in on the
display, each square block is 2 kilometers on each
side. The intensity level reﬂected by the square is
the highest level sampled within the square area.
ECHO TOP – Press the ECHO TOP Softkey to show
the location, elevation, and direction the highest
radar echo. This may not indicate the top of a
storm or clouds, only the highest radar return
echo. ECHO TOPS cannot be displayed along
with NEXRAD and CLOUD TOPS. When ECHO
TOPS is activated, NEXRAD and CLOUD TOPS are
removed. Refer to the Legend for a description of
the ECHO TOPS coding. The display is updated
every 7.5 minutes.
CLD TOP – Press the CLD TOP Softkey to show the
cloud top altitude determined from satellite imagery.
The display is updated every 15 minutes.

Figure 10-9 Weather Data Link Page

NEXRAD – Press the NEXRAD Softkey to show
NEXRAD weather and radar coverage information.
Areas where radar coverage is not available are
shown in grayish-purple. The display is updated
every ﬁve minutes.

10-4

LTNG – Pressing the LTNG Softkey shows the location
of cloud-to-ground lightning strikes. The display is
updated every ﬁve minutes.
NOTE: Strikes depicted represent cloud to ground
strikes within a 2 kilometer radius of the actual
strike location. Therefore, the exact location of
the strike is not displayed.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE
CELL MOV – Pressing the CELL MOV Softkey
shows storm cell movement by displaying an arrow
pointing in the direction of predicted movement.
The display is updated every 12 minutes.
SIG/AIR – Pressing the SIG/AIR Softkey shows
SIGMET and AIRMET information. The display is
updated every 12 minutes.
METAR – Press the METAR Softkey to graphically
display METARs. METARS are shown as colored
ﬂags at airports providing METAR reports. The
display is updated every 12 minutes.
MORE WX – Press the MORE WX Softkey to display
the following group of softkeys for additional
weather control:
SFC – Pressing the SFC Softkey for Surface Analysis
shows current or forecast conditions. Forecasts
are available for intervals of Current, 12, 24, 36,
and 48 hours. Press the softkey corresponding
to the desired forecast. The closest city forecast
information is displayed in the legend. The
display is updated every 12 minutes.
FRZ LVL – Press the FRZ LVL Softkey to display
contour lines for freezing levels. The display is
updated every 12 minutes.
WIND – Press the WIND Softkey to show wind
speed and direction at a selected altitude from
the ground up to 42,000 feet in 3,000 foot
increments. After pressing the WIND Softkey,
press the softkey corresponding to the desired
winds aloft altitude. The display is updated every
12 minutes.
COUNTY – Pressing the COUNTY Softkey provides
speciﬁc public awareness and protection weather
warnings for Tornado, Severe Thunderstorm,
and Flood conditions provided by the National
Weather Service (NWS). The display is updated
every 5 minutes.
190-00384-08 Rev. A

CYCLONE – Pressing the CYCLONE Softkey shows
the current location of cyclones (hurricanes and
tropical storms) and their projected track at
various time intervals. The update rate is every
12 minutes.

Map Panning Information – Weather Data Link
Page
1) Push in the Joystick to display the panning
arrow.
2) Move the Joystick to place the panning arrow on
AIRMETs, TFRs, METARs, or SIGMETs. Press the
ENT Key to display pertinent information for the
selected product.
Note that pressing the ENT Key when panning over
an AIRMET or a SIGMET displays an information box
that displays the text of the report. Panning over
an airport with METAR information does not display
more information but allows the user to press the
ENT Key and select that Airport’s Information Page
to display the text of the report. Pressing the ENT
Key when panning over a TFR displays TFR speciﬁc
information.

Weather Products & Symbols
Figure 10-10 depicts the symbol for each weather
product (read from left to right). When a weather product
is active, the product symbol is displayed in the lower
right of the screen.
• NEXRAD
• Cloud Top/Echo Top
• XM Lightning
• Cell Movement
• SIGMETs/AIRMETs
• METARs
• City Forecast
• Surface Analysis
• Freezing Levels

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10-5

SECTION 10 – HAZARD
AVOIDANCE
• Winds Aloft
• County Warnings
• Cyclone Warnings
Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Figure 10-10 Weather Product Symbols

The XM Information Page in the AUX Page Group
displays the weather products available for the current
subscription. A green box by the weather product means
that it is available.
From within the AUX - XM INFORMATION Page, the pilot
may switch to the AUX - XM RADIO Page by pressing the
RADIO Softkey. Alternatively, the pilot may switch to the AUX
- XM INFORMATION Page from the AUX - XM RADIO Page by
pressing the INFO Softkey.

NOTE: The LOCK Softkey on the AUX - XM
INFORMATION Page is used to save the GDL
69(A) activation data when the XM services
are initially set up. It is not used during normal
operation of the GDL 69(A), but it should have no
adverse effects if inadvertently selected during
ﬂight. Refer to the GDL 69/69A XM Satellite
Radio Activation Instructions (190-00355-04, Rev
E or later) for further information.

Weather Product Age
The age for each of the enabled products is displayed
on the right side of the display. Times are based on GMT
time when the data was assembled on the ground, not the
time the data was received by the XM receiver. When the
age of a weather product has exceeded half of the expiration
time, the product time changes from light blue to amber in
color.

10-6

Weather Product
SIGMETs/AIRMETs
City Forecasts
County Warnings
Cyclone Warnings
Echo Tops
Freezing Levels
METARs
Lightning
NEXRAD
Radar Coverage
Cell Movement
Surface Analysis
TFRs
Winds Aloft
TAFs
Clouds Tops

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

Expires After
(minutes)
60
90
60
60
30
60
90
30
30
30
30
60
60
60
60
60

190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE

10.4 TRAFFIC SYSTEMS
• If Trafﬁc information Service (TIS) is conﬁgured, a
STANDBY, OPERATE, and TNA MUTE Softkey
are displayed.
• If a Trafﬁc Advisory System (TAS) is conﬁgured, a
STANDBY, NORMAL, TEST, and ALT MODE
Softkey are displayed.
• If an ADS-B trafﬁc system is conﬁgured, only the
ALT MODE Softkey is displayed.

has entered Coast Mode. The system maintains the trafﬁc
display (up to 60 seconds) until the next data reception.
If no data is received after 60 seconds, trafﬁc is removed
from the display.
Trafﬁc Advisory, aircraft is 1200’
TNA Mute above & climbing, moving in the Trafﬁc out of
direction of the line
Trafﬁc Mode Status
range

Trafﬁc Information Service (TIS)
NOTE: Trafﬁc Information Service (TIS) is only
available when the aircraft is within the service
volume of a TIS capable terminal radar site.
NOTE: If the G1000 is conﬁgured to use a Trafﬁc
Advisory System (TAS), TIS is not available for
use.

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 second
rectangular page icon.
3) Press the OPERATE Softkey to begin displaying
trafﬁc. ‘OPERATIING’ is displayed in the Trafﬁc
Mode ﬁeld.

Last data update Trafﬁc at same altitude, ProximityTrafﬁc 1200’ above
is older than 6 level ﬂight & moving in the & descending, moving in the
sec. resulting in
direction of the line
direction of the line
Coast Mode

Figure 10-11 Trafﬁc Map Page

Displaying Trafﬁc on the Navigation Map
1) Ensure TIS is operating. With the Navigation Map
displayed, press the MAP Softkey.

4) Press the STANDBY Softkey to place the system in
the Standby Mode. ‘STANDBY’ is displayed in the
Trafﬁc Mode ﬁeld.

2) Press the TRAFFIC Softkey. Trafﬁc is now displayed
on the map.

5) Rotate the Joystick clockwise to display a larger
area or rotate counter-clockwise to display a smaller
area.

When a Trafﬁc Advisory (TA) is displayed, a voice alert
“Trafﬁc” is given.
“Trafﬁc Not Available” is heard whenever TIS service
becomes unavailable. This alert can be muted by pressing
the TNA MUTE Softkey. ‘TNA MUTE ON’ is displayed in
the upper left of the display.

If data is not received for a period longer than 6 seconds,
the age of the present data is displayed in the lower left of
the screen along with the annunciation that the system
190-00384-08 Rev. A

TIS Voice Alert

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-7

SECTION 10 – HAZARD
AVOIDANCE

Trafﬁc Advisory System (TAS) (Optional)
Refer to the Honeywell KTA 870 Pilot’s Guide for a
detailed discussion of the KTA 870 system.
System Self Test
1) Set the range to 2/6 nm.
2) Press the STANDBY Softkey.
3) Press the TEST Softkey.
4) Self test takes approximately eight seconds to
complete. When completed successfully, trafﬁc
symbols are displayed as shown in Figure 10-12
and a voice alert “TAS System Test OK” is heard.
If the self test fails, the system reverts to Standby
Mode and a voice alert “TAS System Test Fail” is
heard.

Figure 10-12 Self Test OK Display

Displaying Trafﬁc on the Trafﬁc Map Page
1) Turn the large FMS Knob to select the Map Page
Group.

3) Press the NORMAL Softkey to begin displaying
trafﬁc. ‘OPERATING’ is displayed in the Trafﬁc Mode
ﬁeld.
4) Press the ALT MODE Softkey to change the altitude
volume. Select the desired altitude volume by
pressing the BELOW, NORMAL, ABOVE, or UNREST
(unrestricted) Softkey. The selection is displayed in
the Altitude Mode ﬁeld.
5) Press the STANDBY Softkey to place the system in
the Standby Mode. ‘STANDBY’ is displayed in the
Trafﬁc Mode ﬁeld.
6) Rotate the Joystick clockwise to display a larger
area or rotate counter-clockwise to display a smaller
area.

Trafﬁc Advisory,
aircraft is 400’ below
Trafﬁc Mode Altitude Mode
& climbing

“Non-Bearing” Trafﬁc (system
is unable to determine bearing),
distance is 8.0 nm, 1190’ above
and descending

Trafﬁc, Out of
Range

Proximity Trafﬁc,
1000’ above &
descending

Figure 10-13 Trafﬁc Map Page

2) Turn the small FMS Knob to select the second
rectangular page icon.
10-8

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE
Displaying Trafﬁc on the Navigation Map
1) Ensure the KTA 870 system is operating. With
the Navigation Map displayed, press the MAP
Softkey.
2) Press the TRAFFIC Softkey. Trafﬁc is now displayed
on the map.
Trafﬁc Advisory

Symbol

Description
Trafﬁc Advisory with directional information. Points in
the direction of the intruder aircraft track.
Trafﬁc Advisory without directional information.
Trafﬁc Advisory out of the selected display range.
Displayed at outer range range ring at proper bearing.
Non-threat trafﬁc with directional information. Points
in the direction of the aircraft track.
Non-threat trafﬁc with no directional information.
Trafﬁc located on the ground with directional
information. Points in the direction of the aircraft
track. Ground trafﬁc is only displayed when own
aircraft is below 1,000 feet AGL or on the ground.
Ground trafﬁc without directional information.
Ground trafﬁc is only displayed when own aircraft is
below 1,000 feet AGL or on the ground.
Non-aircraft ground trafﬁc. Ground trafﬁc is only
displayed when own aircraft is below 1,000 feet AGL
or on the ground.

Non-Bearing
Trafﬁc Off Scale
Trafﬁc Advisories
Banner

Non-Threat
Trafﬁc

Figure 10-14 TAS Trafﬁc on Navigation Map

ADS-B Trafﬁc (Optional)
ADS-B is limited to displaying trafﬁc in the G1000.
Operation is similar to the TAS system discussed
previously, with the exception of symbology. The
following trafﬁc symbols are used to display trafﬁc with
the ADS-B system.

Trafﬁc with directional information, but positional
accuracy is degraded. Points in the direction of the
aircraft track.
Aircraft
Identiﬁcation
(tail number
or Flight ID
number)

Intruder
Aircraft
Heading
(extends in
the direction
of the aircraft
heading)

Relative Altitude
(in this case 1200
feet above own
aircraft)
Altitude Trend
(up arrow
indicates
climbing, down
arrow indicates
descending)

Figure 10-15 Example ADS-B Trafﬁc Advisory
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-9

SECTION 10 – HAZARD
AVOIDANCE

10.5 TERRAIN AND OBSTACLE PROXIMITY
NOTE: Terrain data is not displayed when the
aircraft latitude is greater than 75 degrees north
or 60 degrees south.

4) Rotate the Joystick clockwise to display a larger
area or rotate counter-clockwise to display a smaller
area.

Displaying Terrain and Obstacles on the Terrain
Proximity Page
1) Turn the large FMS Knob to select the Map Page
Group.
2) Turn the small FMS Knob to select the last
rectangular page icon.
3) If desired, press the VIEW Softkey to access the ARC
and 360 Softkeys. When the ARC Softkey is pressed,
a radar-like 120° view is displayed. Press the 360
Softkey to return to the 360° default display.
Figure 10-17 Terrain Proximity Page

Color
RED
YELLOW

Indication
Terrain/Obstacle above or within 100’
below or above aircraft altitude.
Terrain/Obstacle between 100’ and 1000’
below current aircraft altitude.
Aircraft Altitude
100' Threshold

1000'

Unlighted Obstacle
(Height is less than
1000’ AGL)

Lighted Obstacle
(Height is less than
1000’ AGL)

Unlighted Obstacle
(Height is greater than
1000’ AGL)

Lighted Obstacle
(Height is greater than
1000’ AGL)

Figure 10-16 Obstacle Symbols
10-10

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE

Displaying Terrain and Obstacles on the
Navigation Map

Displaying Terrain on the TAWS Page

1) With the Navigation Map displayed, press the MAP
Softkey.
2) Press the TERRAIN Softkey. Terrain and obstacle
proximity is now displayed on the map.

10.6 TERRAIN AWARENESS & WARNING
SYSTEM (TAWS) DISPLAY
(OPTIONAL)
NOTE: Terrain data is not displayed when the
aircraft latitude is greater than 75 degrees north
or 60 degrees south.

1) Turn the large FMS Knob to select the Map Page
Group.
2) Turn the small FMS Knob to select the TAWS
Page.
3) If desired, press the VIEW Softkey to access the ARC
and 360 Softkeys. When the ARC Softkey is pressed,
a radar-like 120° view is displayed. Press the 360
Softkey to return to the 360° default display.
4) Rotate the Joystick clockwise to display a larger
area or rotate counter-clockwise to display a smaller
area.

NOTE: TAWS operation is only available when the
G1000 is conﬁgured for a TAWS-B installation.

Color

Terrain/Obstacle Location

Red

Terrain/Obstacle above or within 100’
below or above aircraft altitude.

Yellow

Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.

Black

Terrain/Obstacle is more than 1000’
below aircraft altitude.
Potential Impact Point
Projected Flight Path

100' Threshold

Unlighted Obstacle

1000'

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-11

SECTION 10 – HAZARD
AVOIDANCE

Figure 10-20 TAWS Page Menu

TAWS Inhibit

Figure 10-18 TAWS Page (360˚ View)

Flying VFR into an area where unique terrain exists
could cause the system to annunciate a nuisance alert.
When TAWS is inhibited, only FLTA and PDA alerts are
disabled.
Inhibit TAWS:
While the TAWS Page is displayed, press the INHIBIT
Softkey. ‘TAWS INHB’ is annunciated in the lower
right of portion of the screen.

Enable TAWS:
If TAWS has been inhibited, from the TAWS Page
press the INHIBIT Softkey. The ‘TAWS INHB”
annunciation is removed.

Figure 10-19 TAWS Page (ARC View)

NOTE: 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.

Enable/Disable Aviation Data
1) While the TAWS Page is displayed, press the MENU
Key.
2) Turn the small FMS Knob to select “Show (or Hide)
Aviation Data”.
3) Press the ENT Key.
10-12

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE

A system test is automatically performed at power-up.
After successful completion of the test, “TAWS System
Test, OK” is heard.
The system test may also be initiated manually, but
only when the aircraft is on the ground. To manually verify
proper operation of the aural and visual annunciations
of the system, perform the following steps.
1) While the TAWS Page is displayed, press the MENU
Key.

2) Turn the small FMS Knob to select ‘Test TAWS’.
3) Press the ENT Key. During the test ‘TAWS TEST’ is
displayed in the center of the TAWS Page.
When all is in working order, “TAWS System Test,
OK” is heard.

Forward Looking Terrain Avoidance (FLTA)
The Forward Looking Terrain Avoidance alert is
composed of two sub-functions:
Reduced Required Terrain Clearance (RTC) and
Reduced Required Obstacle Clearance (ROC)
This provides alerts when the aircraft ﬂight path
is above terrain and/or obstacles, yet is projected to
come within minimum clearance values outlined in the
following table. When an RTC or ROC alert is issued, a
potential impact point is displayed on the TAWS Page as
a yellow or red ‘X’.
Imminent Terrain Impact (ITI) and Imminent
Obstacle Impact (IOI)
This provides alerts when the aircraft is below the
elevation of terrain in the aircraft’s projected path. ITI and
IOI alerts are accompanied by a potential impact point
displayed on the TAWS Page as a yellow or red ‘X’. The
alert is given when the projected vertical ﬂight path is
190-00384-08 Rev. A

calculated to come within minimum clearance altitudes
in the following table.
Phase of Flight

Level Flight

Descending

Enroute

700 ft.

500 ft.

Terminal

350 ft.

300 ft.

Approach

150 ft.

100 ft.

Departure

100 ft.

During the ﬁnal approach phase of ﬂight, RTC/ROC/
ITI/IOI alerts are automatically inhibited when the aircraft
is below 200 feet AGL while within 0.5 nm of the approach
runway or is below 125 feet AGL while within 1 nm of the
runway.

Premature Descent Alert (PDA)
A Premature Descent Alert is issued when the system
detects that the aircraft is signiﬁcantly below the normal
approach path to a runway. The PDA alert mode functions
only during descent to land.
PDA alerting begins when the aircraft is within 15 nm
of the destination airport and ends when the aircraft is
either 0.5 nm from the runway threshold OR is at an altitude of 125 feet AGL while within 1 nm of the threshold.
During the ﬁnal descent, algorithms set a threshold for
alerting based on speed, distance, and other parameters.
700

Height Above Terrain (Feet)

Manual System Test

600

500

400

300

“Too Low, Terrain”

200

100

Runway 1
Threshold

Distance From Destination Airport (nm)

Figure 10-21 PDA Alerting

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-13

The purpose of the Excessive Descent Rate alert is to
provide suitable alerts when the aircraft is determined
to be closing (descending) upon terrain at an excessive
speed. Figure 10-22 displays the correlation between
height above terrain and descent rate, resulting in the two
EDR alerts. EDR alerts have two levels of severity, caution
(sink rate) and warning (pull-up).
6000
5500

Height Above Terrain (Feet)

5000
4500
4000

3500

"
TE
RA

600

400

“DON’T SINK”

200

100

120

140

1000
900
800
700
600
500
400

“DON’T SINK”

300
200
100
0

500

1000

1500

2000

2500

3000

3500

4000

Figure 10-23 Negative Climb Rate

“Five-Hundred” Aural Alert

2500
2000
1500

"PULL UP"

1000
500

2000

4000

6000

8000

10000

12000

Descent Rate

Figure 10-22 Excessive Descent Rate

Negative Climb Rate After Takeoff
Alert (NCR)
The purpose of the Negative Climb Rate After Takeoff
alert is to provide suitable alerts to the pilot when the
system determines that 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.
Figure 10-23 illustrates the envelope for alerts.
10-14

800

Sink Rate (Feet Per Minute)

3000

1000

Altitude Loss (Feet)

Height Above Terrain (Feet)

Excessive Descent Rate Alert (EDR)

Height Above Terrain (Feet)

SECTION 10 – HAZARD
AVOIDANCE

The purpose of the aural alert message “Five-hundred”
is to provide an advisory alert to the air crew that the
aircraft is ﬁve-hundred feet above terrain. When the
aircraft descends within 500 feet of terrain, the aural
message “Five-hundred” is heard. There are no display
annunciations or pop-up alerts that accompany the aural
message.

Displaying Terrain and Obstacles on the
Navigation Map
1) With the Navigation Map displayed, press the MAP
Softkey.
2) Press the TERRAIN Softkey. Terrain and obstacle
proximity are now displayed on the map.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 10 – HAZARD
AVOIDANCE

Pop-up Alerts
When a terrain or obstacle alert is issued, a pop-up
window is displayed on the MFD with the appropriate
alert.

Figure 10-24 TAWS Alert Pop-Up

Press the ENT Key to display the TAWS Page, or press
the CLR Key to remain on the existing page.
Unlighted Obstacle
(Height is less than
1000’ AGL)

Lighted Obstacle
(Height is less than
1000’ AGL)

Unlighted Obstacle
(Height is greater than
1000’ AGL)

Lighted Obstacle
(Height is greater than
1000’ AGL)

Potential Impact Points

Figure 10-25 TAWS Symbols

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-15

SECTION 10 – HAZARD
AVOIDANCE

TAWS Alerts Summary
The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
PFD/MFD TAWS
MFD
Aural Message
Alert Type
Page
Pop-Up Alert
Annunciation
Excessive Descent Rate Warning (EDR)

“Pull Up”

Reduced Required Terrain Clearance
Warning (RTC)

“Terrain, Terrain; Pull Up, Pull Up”
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”

“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”

“Obstacle, Obstacle; Pull Up, Pull Up”
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”

“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”

“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”

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)

Premature Descent Alert Caution (PDA)
Altitude Callout “500”

“Too Low, Terrain”
None

None

Excessive Descent Rate Caution (EDR)

“Sink Rate”

Negative Climb Rate Caution (NCR)

“Don’t Sink”
or
“Too Low, Terrain”

10-16

“Five-Hundred”

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SECTION 10 – HAZARD
AVOIDANCE
The following system status annunciations may also be
issued.
PFD/MFD TAWS
Page
Annunciation

MFD
Pop-Up Alert

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”
“TAWS Available” will be heard when sufﬁcient
GPS signal is re-established.

System Test in progress

None

“TAWS System Test OK”

Alert Type

System Test pass

None

Alert Annunciations
Alert Annunciation

Figure 10-27 TAWS Alert Annunciation on the PFD
Alert Annunciation
Figure 10-26 Alert Annunciation on the TAWS Page

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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

10-17

SECTION 10 – HAZARD
AVOIDANCE

Blank Page

10-18

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 11 – ABNORMAL
OPERATION

SECTION 11: ABNORMAL
OPERATION
11.1 REVERSIONARY MODE
Should a system detected failure occur in either display,
the G1000 automatically enters Reversionary Mode. In
Reversionary Mode, critical ﬂight instrumentation is
combined with engine instrumentation on the remaining
display. Minimal navigation capability is available on the
Reversionary Mode display.

Normal PFD Display

Reversionary display mode can also be manually
activated by the pilot if the system fails to detect a display
problem. The Reversionary Mode is activated manually
by pressing the red DISPLAY BACKUP Button on the
bottom of the audio panel (GMA 1347). Pressing the red
DISPLAY BACKUP Button again deactivates Reversionary
Mode.
NOTE: The Cessna Pilot’s Operating Handbook
(POH) always takes precedence over the
information found in this section.

Normal MFD Display

MFD in Reversionary Mode
Figure 11-1 G1000 Reversionary Mode: Failed PFD

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11-1

SECTION 11 – ABNORMAL
OPERATION

11.2 ABNORMAL COM OPERATION
When a COM tuning failure is detected by the system,
the emergency frequency (121.500 MHz) is automatically
loaded into the active frequency ﬁeld of the COM radio
for which the tuning failure was detected. In the event of
a dual display failure, the emergency frequency (121.500
MHz) automatically becomes the active frequency to the
pilot through the pilot headset.

11.3 UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual
attitude. Only the primary functions are displayed in
these situations.
The following information is removed from the PFD
(and corresponding softkeys are disabled) when the aircraft experiences unusual attitudes:
• Trafﬁc Annunciations
• AFCS Annunciations
• Flight director Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu

11-2

• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
– DME Tuning
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath,
and Vertical Deviation
Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude

Red extreme pitch warning chevrons pointing toward
the horizon are displayed starting at 50 degrees above and
30 degrees below the horizon line.

Figure 11-2 Extreme Pitch Indication

11.4 STORMSCOPE OPERATION WITH
LOSS OF HEADING INPUT
If heading is lost, strikes and/or cells must be cleared
manually after the execution of each turn. This is to
ensure that the strike and/or cell positions are depicted
accurately in relation to the nose of the aircraft.

11.5 HAZARD DISPLAYS WITH LOSS OF
GPS POSITION
If GPS position is lost, or becomes invalid, selected
hazards being displayed on the Navigation Map Page are
removed until GPS position is again established. The
icons in the lower right of the screen, indicating the
selected functions for display, will show an ‘X’, as shown
in Figure 11-3.

Figure 11-3 Loss of Hazard Functions
with Loss of GPS Position

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 11 – ABNORMAL
OPERATION

11.6 DEAD RECKONING
WARNING: 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 compound the relative inaccuracy
of DR Mode. Because of this degraded accuracy,
the crew must maintain position awareness using
other navigation equipment until GPS-derived
position data is restored.

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.
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 navigating in GPS
Mode.

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 11-4. In addition,
‘DR’ is prominently displayed, also in yellow, on the HSI
slightly above and to the right of the aircraft symbol on the
CDI as shown in Figure 11-4. 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.

190-00384-08 Rev. A

Normal navigation using GPS/WAAS source data
resumes automatically once a valid GPS solution is
restored.
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 your 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.

CDI ‘DR’ Indication on PFD

Symbolic Aircraft
(Map pages and Inset Map)

Figure 11-4 Dead Reckoning Indications

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. This data includes the
following:
• 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 and MFD
• Track Bug
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE
values

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

11-3

SECTION 11 – ABNORMAL
OPERATION
Also, while the G1000 is in DR Mode, the autopilot
will not couple to GPS, and both TAWS and Terrain
Proximity 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.

11-4

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

SECTION 12: ANNUNCIATIONS &
ALERTS
NOTE: The Cessna aircraft Pilot’s Operating
Handbook (POH) supersedes information found
in this document.

The G1000 Alerting System conveys alerts to the pilot
using a combination of the following items:
• Annunciation Window: The Annunciation Window
displays abbreviated annunciation text. Text color is
based on alert levels described later in the Alert Levels
Deﬁnitions section. The Annunciation Window
is located to the right of the Altimeter and Vertical
Speed Indicator on the display. All Cessna Nav III
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. Lower priority annunciations are
displayed towards the bottom of the window.
• Alerts Window: The Alerts Window displays alert
text messages. Up to 64 prioritized alert messages
can be displayed in the Alerts Window. 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 pilot can use the large FMS
Knob to scroll through the alert message list.
• 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).
190-00384-08 Rev. A

By pressing the softkey annunciation, the pilot
acknowledges awareness of the alert. The softkey
then returns to the previous ALERTS label. If alerts
are still present, the ALERTS label is displayed in
inverse video (white background with black text).
The pilot can press the ALERTS Softkey a second
time to view alert text messages.
• System Annunciations: Typically, a large red ‘X’
appears in windows when a failure is detected in the
LRU providing the information to the window. See
the G1000 System Annunciations section for more
information.
• Audio Alerting System: The G1000 system issues
audio alert tones when speciﬁc system conditions are
met. See the Alert Levels Deﬁnitions section for more
information.

System
Annunciation
Red ‘X’

Annunciation
Window

Alerts Window

Figure 12-1 G1000 Alerting System

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

ALERTS Softkey
Annunciation

12-1

SECTION 12 – ANNUNCIATIONS
& ALERTS

12.1 ALERT LEVEL DEFINITIONS
The G1000 Alerting System, as installed in Cessna Nav
III aircraft, uses three alert levels.
• WARNING: This level of alert requires immediate
pilot attention. A warning alert is annunciated in
the Annunciation Window and is accompanied
by a continuous aural tone. Text appearing in the
Annunciation Window is RED. A warning alert is
also accompanied by a ﬂashing WARNING Softkey
annunciation, as shown in Figure 12-2. Pressing
the WARNING Softkey acknowledges the presence
of the warning alert and stops the aural tone, if
applicable.
• CAUTION: This level of alert indicates the
existence of abnormal conditions on the aircraft
that may require pilot intervention. A caution alert
is annunciated in the Annunciation Window and is
accompanied by a single aural tone. Text appearing
in the Annunciation Window is YELLOW. A caution
alert is also accompanied by a ﬂashing CAUTION
Softkey annunciation, as shown in Figure 12-3.
Pressing the CAUTION Softkey acknowledges the
presence of the caution alert.

Figure 12-2 WARNING Softkey
Annunciation

Figure 12-3 CAUTION Softkey
Annunciation

Figure 12-4 ADVISORY Softkey
Annunciation

• MESSAGE ADVISORY: This level of alert provides
general information to the pilot. A message
advisory alert does not issue annunciations in the
Annunciation Window. Instead, message advisory
alerts only issue a ﬂashing ADVISORY Softkey
annunciation, as shown in Figure 12-4. Pressing
the ADVISORY Softkey acknowledges the presence
of the message advisory alert and displays the alert
text message in the Alerts Window.

12-2

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

12.2 NAV III AIRCRAFT ALERTS
The following alerts are conﬁgured speciﬁcally for the
Cessna Nav III aircraft. See the Cessna Pilot’s Operating
Handbook (POH) for information regarding pilot
responses.

Safe Operating Annunciation (T182, T206, and
206 with Prop De-Ice Only)
Annunciation Window Text
PROP HEAT

Audio Alert
No Tone

12.3 CO GUARDIAN MESSAGES

WARNING Alerts
Annunciation Window Text
Audio Alert
OIL PRESSURE
Continuous Aural Tone
LOW VOLTS
Continuous Aural Tone*
HIGH VOLTS
Continuous Aural Tone
CO LVL HIGH
Continuous Aural Tone
PITCH TRIM**
No Tone
* Aural tone is inhibited while the aircraft is on the ground.
** KAP 140 installations only

Alerts Window Message
CO DET SRVC – The carbon
monoxide detector needs
service.
CO DET FAIL – The carbon
monoxide detector is inoperative.

Comments
There is a problem within
the CO Guardian that
requires services.
Loss of communication
between the G1000 and
the CO Guardian.

CAUTION Alerts
Annunciation Window Text
LOW VACUUM
LOW FUEL L
LOW FUEL R
STBY BATT

Audio Alert
Single Aural Tone
Single Aural Tone
Single Aural Tone
Single Aural Tone

CAUTION Alerts (T182, T206, and 206 with Prop
De-Ice Only)
Annunciation Window Text
PROP HEAT

190-00384-08 Rev. A

Audio Alert
Single Aural Tone

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12-3

SECTION 12 – ANNUNCIATIONS
& ALERTS

12.4 AFCS ALERTS

System Status Annunciation

System Status Annunciation
The following alert annunciations appear in the AFCS
System Status Annunciation on the PFD.
Figure 12-5 AFCS System Status Annunciation

Condition
Aileron Mistrim Right
Aileron Mistrim Left
Elevator Mistrim Down
Elevator Mistrim Up

Annunciation

Description
Roll servo providing sustained force in the indicated direction

Pitch servo providing sustained force in the indicated direction

Pitch Trim Failure

If AP engaged, take control of the aircraft and disengage AP

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

Preﬂight Test

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

12-4

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

12.5 TAWS ALERTS
The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
PFD/MFD TAWS
MFD
Aural Message
Alert Type
Page
Pop-Up Alert
Annunciation
Excessive Descent Rate Warning (EDR)

“Pull Up”

Reduced Required Terrain Clearance Warning (RTC)

“Terrain, Terrain; Pull Up, Pull Up”
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”

“Obstacle, Obstacle; Pull Up, Pull Up”
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”

“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”

“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”

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)

Premature Descent Alert Caution (PDA)
Altitude Callout “500”

“Too Low, Terrain”
None

None

“Five-Hundred”

Excessive Descent Rate Caution (EDR)

“Sink Rate”

Negative Climb Rate Caution (NCR)

“Don’t Sink”
or
“Too Low, Terrain”

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12-5

SECTION 12 – ANNUNCIATIONS
& ALERTS
The following system status annunciations may also be issued.
PFD/MFD TAWS
Page
Annunciation

MFD
Pop-Up Alert

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”
“TAWS Available” will be heard when sufﬁcient
GPS signal is re-established.

System Test in progress

None

“TAWS System Test OK”

Alert Type

System Test pass

None

12.6 OTHER G1000 AURAL ALERTS
Aural Alert

Description

“Minimums, minimums” The aircraft has descended below the preset barometric minimum descent
altitude.
“Vertical track”

12-6

The aircraft is one minute from Top of Descent. Issued only when vertical
navigation is enabled.

“Trafﬁc”

The Trafﬁc Information Service (TIS) or ADS-B trafﬁc system has issued a Trafﬁc
Advisory alert

“Trafﬁc not available”

The aircraft is outside the Trafﬁc Information Service (TIS) or ADS-B coverage area.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

12.7 G1000 SYSTEM ANNUNCIATIONS
When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on areas associated with the failed data.
Refer to the POH for additional information regarding pilot responses to these annunciations.
NOTE: Upon power-up of the G1000 system, certain boxes remain invalid as G1000 equipment begins to
initialize. All boxes should be operational within one minute of power-up. Should any box continue to remain
ﬂagged, the G1000 system should be serviced by a Garmin-authorized repair facility.

System Annunciation

Comment

Attitude and Heading Reference System is aligning.

Display system is not receiving attitude information from the AHRS.

Indicates a conﬁguration module failure.

This annunciation is only seen 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.

Display system is not receiving airspeed input from air data computer.

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12-7

SECTION 12 – ANNUNCIATIONS
& ALERTS

System Annunciation

Comment

Display is not receiving altitude input from the air data computer.

Display is not receiving vertical speed input from the air data computer.

Display is not receiving valid heading input from AHRS.
Display is not receiving valid transponder information.
‘LOI’ Indicates Loss of Integrity of GPS information. GPS information is
either not present or is invalid for navigation use. ‘DR’ may also be seen
indicating that GPS is in Dead Reckoning Mode. Note that AHRS utilizes GPS
inputs during normal operation. AHRS operation may be degraded if GPS
signals are not present (see AFMS).
Other Various Red X Indications

12-8

A red ‘X’ through any other display ﬁeld, such as engine instrumentation
ﬁelds, indicates that the ﬁeld is not receiving valid data.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS
A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible ﬂags and the
responsible LRUs.
GIA 63/63W
Integrated Avionics
Units

GIA 63/63W
Integrated Avionics
Units
GDC 74A Air Data
Computer

GRS 77 AHRS
Or
GMU 44
Magnetometer

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

GIA 63/63W
Integrated Avionics
Units

GDC 74A Air Data
Computer
Figure 12-6 G1000 System Failure Annunciations

GTX 33 Transponder
Or
GIA 63/63W
Integrated Avionics
Units

12.8 G1000 SYSTEM MESSAGE ADVISORIES
This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU
function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in
the G1000 System Annunciation section.
NOTE: This section provides information regarding G1000 message advisories that may be displayed by the
system. Knowledge of the aircraft, systems, ﬂight conditions, and other existing operational priorities must
be considered when responding to a message. Always use sound pilot judgment. The Cessna aircraft Pilot’s
Operating Handbook (POH) takes precedence over any conﬂicting guidance found in this section.

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12-9

SECTION 12 – ANNUNCIATIONS
& ALERTS

MFD & PFD Message Advisories
Message
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] Key
is stuck.
MFD1 KEYSTK – MFD [key name] Key
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
12-10

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.
The PFD and/or MFD self-test has detected a problem. The G1000 system should
be serviced.

The PFD and/or MFD has incorrect software installed. The G1000 system should
be serviced.

The PFD and/or 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.
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.
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.
The PFD1 conﬁguration module backup memory has failed. The G1000 system
should be serviced.
The PFD and/or MFD voltage is low. The G1000 system should be serviced.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

Database Message Advisories
Message
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.

190-00384-08 Rev. A

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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

12-11

SECTION 12 – ANNUNCIATIONS
& ALERTS

Database Message Advisories (Cont.)
Message
MFD1 DB ERR – MFD1 airport terrain
database missing.
PFD1 DB ERR – PFD1 airport terrain
database missing.
MFD1 DB ERR – MFD1 SafeTaxi
database error exists.
PFD1 DB ERR – PFD1 SafeTaxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
MFD1 DB ERR – MFD1 FliteCharts
database error exists.
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.

12-12

Comments
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 SafeTaxi 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.
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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

GMA 1347 Message Advisories
Message
GMA1 FAIL – GMA1 is inoperative.
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.
The audio panel has incorrect software installed. The G1000 system should be
serviced.
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.

GIA 63 Message Advisories
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.
190-00384-08 Rev. A

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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

12-13

SECTION 12 – ANNUNCIATIONS
& ALERTS

GIA 63 Message Advisories (Cont.)
Message
Comments
MANIFEST – GIA1 software mismatch,
communication halted.
The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should
MANIFEST – GIA2 software mismatch, be serviced.
communication halted.
COM1 TEMP – COM1 over temp.
The system has detected an over temperature condition in COM1 and/or COM2. The
Reducing transmitter power.
transmitter is operating at reduced power. If the problem persists, the G1000 system
COM2 TEMP – COM2 over temp.
should be serviced.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
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.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or
is stuck.
“pressed”) position. Press the PTT switch again to cycle its operation.
COM2 PTT – COM2 push-to-talk key
If the problem persists, the G1000 system should be serviced.
is stuck.
COM1 RMT XFR – COM1 remote
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) positransfer key is stuck.
tion. Press the transfer switch again to cycle its operation. If the problem persists,
COM2 RMT XFR – COM2 remote
the G1000 system should be serviced.
transfer key is stuck.
RAIM UNAVAIL – RAIM is not
GPS satellite coverage is insufﬁcient to perform Receiver Autonomous Integrity
available from FAF to MAP waypoints.
Monitoring (RAIM) from the FAF to the MAP waypoints.
LOI – GPS integrity lost. Crosscheck
Loss of GPS integrity monitoring.
with other NAVS.
GPS NAV LOST – Loss of GPS navigaLoss of GPS navigation due to insufﬁcient satellites.
tion. Insufﬁcient satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.

12-14

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

GIA 63 Message Advisories (Cont.)
Message
Comments
ABORT APR – Loss of GPS navigation.
Abort approach due to loss of GPS navigation.
Abort approach.
TRUE APR – True north approach.
Displayed after passing the ﬁrst waypoint of a true north approach when the nav
Change hdg reference to TRUE.
angle is set to ‘AUTO’.
GPS1 FAIL – GPS1 is inoperative.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is
unavailable. The G1000 system should be serviced.
GPS2 FAIL – GPS2 is inoperative.
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.

190-00384-08 Rev. A

A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be serviced.

A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be serviced.
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.
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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

12-15

SECTION 12 – ANNUNCIATIONS
& ALERTS

GIA 63W Message Advisories
Message
GIA1 CONFIG – GIA1 conﬁguration
error. Conﬁg service req’d.
GIA2 CONFIG – GIA2 conﬁguration
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.

12-16

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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

GIA 63W Message Advisories (Cont.)
Message
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.
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.

190-00384-08 Rev. A

Comments
The system has detected an over temperature condition in COM1 and/or COM2.
The transmitter is operating 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.
GPS integrity is insufﬁcient for the current phase of ﬂight.
Loss of GPS navigation due to insufﬁcient satellites.
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Vertical guidance generated by WAAS is unavailable, use LNAV only minimums.
Displayed after passing the ﬁrst waypoint of a true north approach when the nav
angle is set to ‘AUTO’.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

12-17

SECTION 12 – ANNUNCIATIONS
& ALERTS

GIA 63W Message Advisories (Cont.)
Message
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.

Comments
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may
still be available. The G1000 system should be serviced.

A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may
still be available. The G1000 system should be serviced.
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.
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.

GEA 71 Message Advisories
Message
GEA1 CONFIG – GEA1 conﬁguration
error. Conﬁg service req’d.
MANIFEST – GEA1 software
mismatch, communication halted.

12-18

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.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

GTX 33 Message Advisories
Message
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 Message Advisories
Message
AHRS1 TAS – AHRS1 not receiving
airspeed.

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
GPS source.
G1000 system should be serviced when possible.
The #1 AHRS is not receiving any or any useful GPS information. Check AFMS
AHRS1 GPS – AHRS1 not receiving
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
backup GPS information.
be serviced.
AHRS1 GPS – AHRS1 operating
The #1 AHRS is operating exclusively in no-GPS mode. The G1000 system should
exclusively in no-GPS mode.
be serviced.
AHRS1 SRVC – AHRS1 Magnetic-ﬁeld The #1 AHRS earth magnetic ﬁeld model is out of date. Update magnetic ﬁeld
model needs update.
model when practical.
GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for approved AHRS operation. Heading
South, no magnetic compass.
is ﬂagged as invalid.
MANIFEST – GRS1 software
The #1 AHRS has incorrect software installed. The G1000 system should be
serviced.
mismatch, communication halted.

190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

12-19

SECTION 12 – ANNUNCIATIONS
& ALERTS

GMU 44 Message Advisories
Message
HDG FAULT – AHRS1 magnetometer
fault has occurred.
MANIFEST – GMU1 software
mismatch, communication halted.

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.
The GMU 44 has incorrect software installed. The G1000 system should be
serviced.

GDL 69A Message Advisories
Message
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
MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The G1000 system should be
communication halted.
serviced.

GDC 74A Message Advisories
Message
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
MANIFEST – GDC1 software
mismatch, communication halted.

12-20

Comments
The GDC 74A is reporting that the altitude error correction is unavailable.
The GDC 74A is reporting that the airspeed error correction is unavailable.
The GDC 74A has incorrect software installed. The G1000 system should be
serviced.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

SECTION 12 – ANNUNCIATIONS
& ALERTS

Miscellaneous Message Advisories
Message
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.
FPL TRUNC – Flight plan has been
This occurs when a newly installed aviation database eliminates an obsolete
truncated.
approach 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
than 10 minutes.
within 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.
190-00384-08 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

12-21

SECTION 12 – ANNUNCIATIONS
& ALERTS

Miscellaneous Message Advisories (Cont.)
Message
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.
VNV – Unavailable. Unsupported leg
type in ﬂight plan.
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.
SCHEDULER [#] – .
12-22

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/W has failed.
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°.
Message criteria entered by the user.

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

INDEX
A
Abnormal COM operation 11-2
Activate a ﬂight plan 8-3
Active ﬂight plan 8-2
ADF 1-6, 1-7, 5-3
ADS-B RR-1, 10-7, 10-9, 12-6
AFCS 12-4
Age 10-6
AHRS 12-19, 12-20
Aircraft alerts 12-3
AIRMET 10-5
Airport frequency 7-25
Airport information 7-21
Airspace alerts 7-29
Airspeed indicator 2-3
Airspeed Reference 6-8
Airspeed trend vector 2-3
Airways 8-5
Alerting system 12-1
Alerts 12-1
Alert levels 12-2
Alert Pop-Up 10-15
ALT 1-4, 1-7, 2-4, 6-4, 6-6, 6-13, 7-19,
10-8
Altitude alerting 2-4
Altitude constraints 1-10, 7-12
Altitude hold 1-4
Altitude Hold Mode 6-6
Altitude mode 10-8
Altitude Reference 6-6, 6-13
Altitude restrictions 1-11
Altitude trend vector 2-4
Altitude volume 10-8
ALT Knob 1-4
Ammeter 3-2, 3-8
AP 1-4
Approach
ILS 6-31
Missed 6-33
WAAS 6-32
Approaches 9-2
Approach activation 4-4
Approach markers
190-00384-08 Rev. A

Signal augmentation 5-2
Approach Mode 6-20, 6-31
Approach Mode, AFCS 6-32
AP DISC Switch 6-1, 6-34
Arrivals 9-1
Assist 3-4, 3-6, 3-7
Attitude indicator 2-3
Audio alerting system 12-1
Audio panel 4-3, 5-1
Audio panel controls
ADF 5-3
DME 5-3
NAV1 5-3
NAV2 5-3
Aural alerts 12-6
Auto-tuning 4-4
Automatic Flight Control System (AFCS)
Status Annunciations 6-34
Status Box 6-2
Automatic squelch 4-3
Autopilot 6-22–6-23
Autopilot disconnect 6-16, 6-23

COM frequency window 4-1
COM Knob 4-3
Controls 1-2
Control Wheel Steering (CWS) 6-23
Create a new user waypoint 8-1
CWS Button 6-1, 6-5 – 6-10, 6-13
– 6-18, 6-20 – 6-23
Cyclones 10-5
Cylinder Head Temperature 3-1, 3-4

D
Databases 1-12
Dead Reckoning 2-12, 11-3, 12-8
Departures 9-1
Direct-to 7-1 – 7-5, 7-11, 7-12, 8-8
DME 1-7
DR 2-12
DR mode 11-3, 11-4
Dual CDU failure 11-2

Backcourse Mode 6-21
Barometric minimum 2-8
Base reﬂectivity 10-4
BRG1 2-11
BRG2 2-11

ECHO TOPS 10-4
Edit a ﬂight plan 8-7
EDR 10-14
Engine Hours 3-2, 3-8
Engine Leaning 3-6
Engine Page 3-1
Excessive Descent Rate 10-14
Exhaust Gas Temperature 3-1, 3-4

CAUTION 12-2
Caution alerts 12-3
CDI 2-9, 2-11, 7-3, 7-6, 7-12, 7-16,
7-20, 9-2, 12-22
Cell 10-2
Cell mode 10-2
Cell movement 10-5
Cloud Tops 10-4
CLR 1-3, 3-8
Coast mode 10-7
Code selection 4-5
Command Bars, ﬂight director 6-2

FD 1-4
Five-Hundred Aural Alert 10-14
FLC 1-4
Flight director 6-2–6-3
Pitch modes 6-3–6-9
Roll modes 6-17–6-19
Flight ID 4-5
Flight level change 1-4
Flight Level Change Mode 6-28, 6-30
Flight Level Change Mode (FLC) 6-8
Flight Plan Catalog 9-1, 9-2
FLTA 10-13

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

Index-1

INDEX
Forward Looking Terrain Avoidance
10-13
Freezing level 10-5
Frequency toggle key 1-3, 4-3
Fuel
Calculations 3-7
Flow totalizer 3-7
Remaining 3-8
Used 3-8
Fuel Flow 3-1, 3-3, 3-4, 3-8
Fuel Quantity 3-2, 3-4, 3-8

Key(s) 1-4

Nav/Com controls 4-1
NAV1 5-3
NAV2 5-3
Navigation 7-1
Navigation database 1-10, 1-11, 7-5
Navigation Mode 6-19–6-20, 6-26–627
Navigation status window 2-2
NAV frequency window 4-1
NCR 10-14
Nearest Airports Page 7-21, 7-25 – 729, 8-1
Nearest ARTCC & FSS frequencies 7-28
Negative Climb Rate After Takeoff
10-14
NEXRAD 1-9, 10-3 – 10-6
Non-path descent 6-12, 6-30–6-31

GA Switch (Go-Around) 6-1
Glidepath 2-2, 2-6, 7-19
Glidepath Mode 6-14, 6-20
Glidepath Mode (GP) 6-32
Glideslope 2-6, 7-19
Glideslope Mode 6-15, 6-20, 6-31
GMA 1347 1-1
Go Around Mode 6-33–6-34
Go Around Mode (GA) 6-16

Leaning 3-7
Leaning, Engine 3-4
Lean Display 3-1, 3-4, 3-5, 3-6
Lighted obstacle 10-15
Lightning 1-5, 1-9, 10-2, 10-3, 10-4
LNAV 2-6, 7-5
Load approach 8-6
Load a VOR frequency 7-27
Load departure 8-6
Load the frequency for a controlling
agency 7-29
Load the nearest ARTCC frequency
7-28
LOI 2-11
LOW ALT 2-5
Low Altitude 2-5
LPV 2-6, 6-24, 7-5, 7-20

Heading indication 2-9
Heading Select 1-3, 1-4
Heading Select Mode 6-18
Headset(s) 5-3
Horizontal situation indicator 2-8
HSI 2-8
Hurricanes 10-5

Manifold Pressure 3-1, 3-3, 3-4, 3-6,
3-8, 3-10
Manual Electric Trim (MET) 6-22
MAP 7-1
Map panning 10-5
Marker beacon 2-7
Message advisories 12-2, 12-10 – 1215, 12-17 – 12-22
METAR 10-3, 10-5
Metric display 2-4
MET Switch (Manual Electric Trim) 6-1
MFD 1-1, 4-4
Minimums 12-6
Missed approach 6-33
MKR/MUTE 5-2, 5-4
Mode S 4-4
Mode selection softkeys 4-5
Morse code identiﬁer 4-3

I
ID RR-1, 1-3, 4-2, 4-3, 4-6
IDENT function 4-5
ILS approach 6-31
Imminent Terrain Impact 10-13
Impact point 10-13
Inhibit 10-12
Interrogations 4-5
IOI 10-13, 10-16, 12-5
ITI 10-13
Index-2

O
OBS 2-12
Obstacles 10-10, 10-15, 12-12, 12-16
Oil Pressure 3-1, 3-8
Oil Temperature 3-1, 3-8
Operation 5-2
Optional
NAV radios 4-3
Overspeed protection, autopilot 6-35

P
Page group icon 1-9
PDA 10-13
Peak, Cylinder 3-7–3-8
Peak temperature 3-4, 3-7
PFD 1-1, 4-1, 4-4
Pitch hold 1-4
Pitch Hold Mode (PIT) 6-5
Pitch modes, ﬂight director 6-3–6-9
Pitch Reference 6-5
Premature Descent Alert 10-13
Procedures
GFC 700 6-24–6-36
Procedure examples, AFCS 6-24–6-31

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

INDEX
R

Red pointer 2-3
Remove departure, arrival, or approach
8-6
Replies 4-5
Required Vertical Speed 2-6, 7-15
Required Vertical Speed Indicator 7-15
Reversionary mode 5-1, 11-1
ROC 10-13, 10-16, 12-5
Roll Hold Mode (ROL) 6-17
Roll modes, ﬂight director 6-17–6-20
Roll Reference 6-18
RTC 10-13
RVSI 7-15, 7-16
RX indicator 4-3
R indication 4-5

TA 10-7
Tachometer 3-1, 3-4, 3-8
TAF 10-3
TAS 10-7, 10-8, 10-9, 12-19
TAWS 10-11 – 10-13, 10-15 – 10-17,
12-5, 12-6
TAWS-B 10-11
TAWS system test 10-13
Temperature
Peak Cylinder 3-7
Turbine Inlet 3-7
Terrain 10-10, 10-11, 10-15, 10-17,
11-2, 12-12
TIS 10-7
TNA Mute 10-7
TOD 7-15, 7-18
Top of Descent 7-15
Tornado 10-5
Trafﬁc advisory 10-7, 10-8, 10-9,
10-17
Trafﬁc map page 10-7, 10-8, 10-9,
10-11, 10-14
Transponder 4-4
Transponder standby mode 4-4
Transponder Status bar 4-5
Trim adapter 6-22
Tropical storms 10-5
Turbine Inlet Temperature 3-1, 3-4, 3-7
Turbine Inlet Temperature (TIT) 3-7
TX 4-3, 7-23

S
Secure Digital (SD) card 1-12
Selected Altitude 6-6, 6-10, 6-13
Selected Altitude Capture Mode 6-6,
6-10, 6-13
Selected Course 6-20, 6-21
Selected Heading 6-18
Selected vertical speed 2-7
Servos 6-22
Severe thunderstorm 10-5
SIGMET 10-5
Slip/Skid indicator 2-3
Softkey function (MFD) 1-5, 1-8
Speed ranges 2-3
SQ 1-3, 4-2, 4-3, 5-1, 5-4
Squelch 5-4
STBY Softkey 4-4
Store Flight Plan 8-6
Stormscope lightning data 1-5, 1-9,
10-1, 10-2, 10-3
Strike 10-2
Strike mode 10-2
System annunciations 12-1
System message advisories 12-9

190-00384-08 Rev. A

U
Unlighted obstacle 10-15

V
Vacuum Pressure 3-1, 3-8
VDI 7-15, 7-16
Vertical Descent Indicator 7-15
Vertical Deviation 2-2, 2-6
Vertical deviation guidance 1-10, 1-11
Vertical navigation 1-10, 1-11

Vertical Navigation ﬂight control 610–6-14
Vertical Path Tracking Mode 6-10–611, 6-29
Vertical speed 1-4, 2-7
Vertical Speed Bug 2-7
vertical speed guidance 1-10, 1-11
Vertical Speed Mode 6-7
Vertical Speed Reference 6-7
Vertical track 12-6
VHF 4-1
VNAV 1-11, 7-1 – 7-4, 12-22
VNAV Target Altitude 6-10–6-13
VNAV Target Altitude Capture Mode
6-13
VNV 1-10, 1-11, 7-15
Voice alerts 12-3
VOL/PUSH ID 4-2
VOL/PUSH SQ 4-2, 4-3
Voltmeter 3-2, 3-8
Volume/squelch 5-4
VS 1-4
VSI 7-16
Vspeeds 2-3

W
WAAS 2-6, 6-24, 7-5, 12-16
WAAS precision approach 6-32
WARN 2-11, 2-12
WARNING 12-2
Warning alerts 12-3
Weather data link page 10-4
Weather product symbol 10-5
Weather product symbols 10-6
Weather warnings 10-5
Wind direction 10-5
Wind speed 10-5
Wings level 6-16, 6-18

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

Index-3

INDEX

Blank Page

Index-4

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-08 Rev. A

Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282
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
Hounsdown Business Park
Southampton, SO40 9RB, U.K.
p: 44/0870.8501241 f: 44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com

190-00384-08 Rev. A

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Garmin Software Version 0563 05 Cockpit Reference Guide 190 00384 08_0A

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