Garmin Software Version 0424 01 Cockpit Reference Guide 190 00450 00_0B

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G1000

cockpit reference guide
for Mooney M20M & M20R

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

COPYRIGHT
Copyright © 2004 Garmin Ltd. or its subsidiaries. All rights reserved.
This Cockpit Reference Guide reﬂects the operation of System Software version 0424.01 for Mooney M20M and M20R 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., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K.
Tel: 44/1794.519944
Fax: 44/1794.519222
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® is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000™, GMA™, GTX™ and Spell’N Find™ 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..

November 2004

190-00450-00 Rev. B

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Printed in the U.S.A.

RECORD OF REVISIONS

Revision Date of Revision Affected Pages
A
10/19/04
i - xii,
1 - 114
B

11/02/24

i - xii,
1 - 114

Description
Production Release
Update SW number.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

ECO Number
27851
28077

TABLE OF CONTENTS
Copyright

Record of Revisions

Table of Contents

iii

List of Figures

List of Tables

viii

WARRANTY

Warnings and Cautions

Section 1: Introduction

1
1.1 G1000 Controls .......................................................... 2
1.2 Secure Digital Cards ................................................. 4
1.3 System Power-up ...................................................... 4
PFD Power Up
5
MFD Power Up
5
1.4 Initial Operations ...................................................... 6
1.5 Backlighting ............................................................... 6
1.6 Reversionary Mode .................................................. 6

Section 2: Primary Flight Display

9
2.1 Backlighting ............................................................. 12
2.2 Softkey Function ..................................................... 13
2.3 Flight Instruments .................................................. 17
Airspeed Indicator
17
Speed Indication
17
Speed Ranges
17
Airspeed Trend Vector
17
Vspeed References
17
True Airspeed Box
17
Attitude Indicator
18
Pitch Indication
18
Roll Indication
19
Slip/Skid Indication
19
Altimeter
20
Altitude Values
20
Altitude Reference Bug
20
Altitude Trend Vector
20
Altitude Reference Box
20
Barometric Setting Box
20
Altitude Alerting
21

Metric Display
22
Vertical Deviation/Glideslope Indicator
22
Marker Beacon Annunciations
22
Vertical Speed Indicator
23
Vertical Speed Pointer
23
Horizontal Situation Indicator
24
Heading Indication
25
Turn Rate Indicator
25
Course Deviation Indicator
25
Bearing Pointers and Information Windows
26
Navigation Source
27
2.4 Communication, Navigation & Surveillance ..... 28
Communication Frequency Window
28
Navigation Frequency Window
28
Navigation Status Bar
29
Transponder Status Bar
30
Transponder Operation
30
Transponder Code Selection
30
2.5 Alerts and Annunciations ...................................... 30

Section 3: Audio Panel

31
3.1 Front Panel Controls............................................... 31
Microphones
33
Mono/Stereo Headsets
33
Unmuted/Unswitched Inputs
33
3.2 Unit Operation ......................................................... 34
Power-up Settings
34
Fail-safe Mode
34
Selecting Keys
34
Deselecting Keys
34
Lighting
34
Transceiver Keys
35
Pressing a COM MIC Key
35
Pressing a COM Key
35
Keying a Microphone
35
COM Swap
36
Split COM
36
PA Function
36
Split COM and PA
37
Speaker Output
37
3.3 Marker Beacon Receiver ....................................... 38
Description and Operation
38
Marker Beacon Signal Augmentation
38

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

iii

TABLE OF CONTENTS
3.4 Radio Inputs ............................................................. 40
3.5 Intercom System (ICS) Isolation .......................... 41
PILOT Mode
41
COPILOT Mode
41
CREW Mode
41
ALL Mode
41
3.6 Volume/Squelch Control ........................................ 42
Intercom VOL/SQ State
43
Intercom Volume Control
43
Intercom Squelch Threshold Control
43
3.7 Display Backup Mode............................................. 44

Section 4: Multi Function Display

45
4.1 Introduction ............................................................. 45
4.2 MFD Softkeys ........................................................... 45
4.3 Engine Indication System Window ..................... 47
ENGINE Page
47
Manifold Pressure Gauge
47
Tachometer
47
Fuel Qty Indicator
47
Fuel Flow Indicator (Normally Aspirated)
49
Fuel Pressure Indicator (Turbocharged Only)
49
Oil Pressure Indicator
49
Oil Temperature Indicator
49
EGT Indicator (Normally Aspirated)
49
TIT Indicator (Turbocharged Only)
49
CHT Indicator
49
Voltmeter
49
Ammeter
49
Rudder Trim Indicator
49
Elevator Trim Indicator
49
Flaps Position Indicator
49
4.3 MFD Page Groups.................................................... 50
Working With Menus
51
4.4 Navigation Map Page ............................................ 52
Navigation Map Page Operations
52
Changing the Map Orientation
54
Clearing Lightning Data
54
Selecting a Map Range
54
Using the Auto Zoom Feature
54
Identifying Aviation Map Data
54
Decluttering the Map
55
Map Panning
55

4.5

4.6

4.7

4.8

Displaying Topographic Data on the Navigation Map
Page
57
Displaying Terrain Data on the Navigation Map Page 57
Displaying Trafﬁc on the Navigation Map Page
57
Displaying Lightning Data on the
Navigation Map Page
58
Lightning Data Display Range
59
MFD Navigation Status Window
59
Navigation Map Page Menu
60
First Option: ‘MAP SETUP’
60
Map Group
60
Orientation
60
Trafﬁc Map Page ..................................................... 61
TIS Symbology
63
Trafﬁc Map Page Operations
63
Power-Up Test
63
Changing the Map Range
63
Operating Mode
64
TIS Audio Alert
64
TIS Trafﬁc Status
65
Trafﬁc Banner
65
Weather Map Page ................................................. 66
Weather Display Information
67
Weather Map Page Operations
67
Lightning Strike Symbols
67
Terrain Proximity Page .......................................... 68
Terrain Proximity Page Operations
68
Displaying Obstacle Data
69
Obstacle Shapes
69
Navigation Map Display Conditions
69
Direct-To Navigation .............................................. 70
Direct to Navigation Operations
71
Selecting a Direct-to Waypoint
71
Selecting a Direct-to Destination by Facility or City
Name
71
Selecting a Direct-to Destination from the Active Flight
Plan
71
Selecting a Nearest Airport as a Direct-to Destination72
Shortcuts
72
Canceling Direct-to Navigation
73
Specifying a Course to a Waypoint
74

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

TABLE OF CONTENTS
4.9 Flight Plans ............................................................... 75
Active Flight Plan Page
75
Active Flight Plan Page Operations
75
Create a New Flight Plan
75
Delete a Waypoint
77
Remove Departure, Arrival, or Approach
77
Flight Plan Catalog Page
78
Flight Plan Catalog Page Operations
79
Activate a Flight Plan
79
Stop Navigating a Flight Plan
79
Invert and Activate a Flight Plan
80
Copy a Flight Plan
80
Delete a Flight Plan
80
Delete All Flight Plans
81
Point-n-Shoot Flight Plan Creation Feature
81
4.10 Procedures ................................................................ 82
Arrivals and Departures
82
Approaches
83
G1000 Navigational Guidance for Approaches
83
Selecting Approaches
84
GPS Approach Examples
86
No Procedure Turn
86
Flying the Missed Approach
88
Flying the Procedure Turn
90
Flying the DME ARC
92
Flying a Holding Pattern
94

Appendix A

97
A.1 Introduction ............................................................. 97
A.2 Alert Levels .............................................................. 98
A.3 Mooney Speciﬁc Aircraft Alerts ........................... 99
Audio Alerts
99
Voice Alerts
99
A.4 G1000 System Annunciations ............................. 100
A.5 G1000 System Message Advisories ................... 103
MFD & PFD Message Advisories
103
Database Message Advisories
104
GMA 1347 Message Advisories
104
GIA 63 Message Advisories
105
GEA 71 Message Advisories
107
GTX 33 Message Advisories
107
GRS 77 Message Advisories
108
GMU 44 Message Advisories
108
GDC 74A Message Advisories
109
Miscellaneous Message Advisories
109

Index

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

111

LIST OF FIGURES

LIST OF FIGURES
Figure 1-1 G1000 Controls........................................................ 2
Figure 1-2 G1000 Power-Up ..................................................... 5
Figure 1-3 G1000 Normal Mode............................................... 7
Figure 1-4 G1000 Reversionary Mode: Failed PFD .................. 7
Figure 2-1 Default PFD Information ........................................ 10
Figure 2-2 Additional PFD Information ................................... 11
Figure 2-3 PFD Setup Menu .................................................... 12
Figure 2-4 PFD Softkeys (1 of 2).............................................. 14
Figure 2-4 PFD Softkeys (2 of 2).............................................. 15
Figure 2-5 Airspeed Indicator .................................................. 17
Figure 2-6 Red Pointer at Vne ................................................. 17
Figure 2-7 Attitude Indicator ................................................... 18
Figure 2-8 Attitude Indicator Nose High ................................. 19
Figure 2-9 Attitude Indicator Nose Low .................................. 19
Figure 2-10 Altimeter ............................................................... 20
Figure 2-11 Colors Associated with the Altitude Alerter ........ 21
Figure 2-12 Altimeter within 1,000 ft. of Reference Altitude 21
Figure 2-13 Altimeter within 200 ft. of Reference Altitude ... 21
Figure 2-14 Altimeter (Metric) ................................................. 22
Figure 2-16 Marker Beacon and Vertical Deviation................ 22
Figure 2-16 Vertical Speed Indicator ....................................... 23
Figure 2-17 ARC HSI ................................................................ 24
Figure 2-18 Horizontal Situation Indicator ............................. 24
Figure 2-19 Selected Heading Box .......................................... 25
Figure 2-20 Turn Rate Indicator and Trend Vector .................. 25
Figure 2-21 Selected Course Box ............................................ 25
Figure 2-22 HSI with Bearing Information .............................. 26
Figure 2-23 BRG1 Information Window .................................. 26
Figure 2-24 BRG2 Information Window ................................. 26
Figure 2-25 GPS INTEG, GPS SUSP, NAV1 and NAV2 ............ 27
Figure 2-26 Communication Frequency Window ................... 28
Figure 2-27 Navigation Frequency Window ........................... 28
Figure 2-28 Navigation Status Bars ........................................ 29
Figure 2-29 Navigation Status Bar Message .......................... 29
Figure 2-30 Transponder Status Bar ........................................ 30
Figure 3-1 Front Panel Controls............................................... 32
Figure 3-2 Transceivers............................................................. 35

Figure 3-3 Split COM, PA and Speaker ................................... 37
Figure 3-4 Marker Beacon ....................................................... 38
Figure 3-5 Marker Beacon Signal Indicator Lights on the PFD39
Figure 3-6 Aircraft Radios ........................................................ 40
Figure 3-7 ICS Isolation ........................................................... 41
Figure 3-8 Reversionary Mode ................................................ 44
Figure 4-2 MFD Softkeys .......................................................... 46
Figure 4-3 ENGINE Page (Normally Aspirated) ....................... 48
Figure 4-4 ENGINE Page (Turbocharged) ................................ 48
Figure 4-5 Page Group Window .............................................. 50
Figure 4-6 Page Title Window .................................................. 50
Figure 4-6 Menu With Options ................................................ 51
Figure 4-7 Menu With No Options .......................................... 51
Figure 4-8 Navigation Map Page ............................................ 53
Figure 4-9 Navigation Map Range .......................................... 54
Figure 4-10 Navigation Map Panning ..................................... 56
Figure 4-11 TRAFFIC, TOPO and TERRAIN Softkeys................ 57
Figure 4-12 Topography Scale ................................................. 58
Figure 4-13 MFD Navigation Status Window ......................... 59
Figure 4-14 Navigation Map Page Menu Options ................. 60
Figure 4-15 Trafﬁc Map Page................................................... 62
Figure 4-16 Weather Map Page ............................................. 66
Figure 4-17 Terrain Scale .......................................................... 68
Figure 4-18 Direct-to Page ....................................................... 70
Figure 4-19 Flight Plan Waypoint Direct-to ............................ 71
Figure 4-20 Nearest Airport Direct-to ...................................... 73
Figure 4-21 Manual Course Direct-to ..................................... 74
Figure 4-22 New Flight Plan.................................................... 76
Figure 4-23 Remove Waypoint Conﬁrmation ......................... 77
Figure 4-24 Removing an Approach ....................................... 78
Figure 4-25 Flight Plan Catalog Page ..................................... 78
Figure 4-26 Flight Plan Catalog Page Options ....................... 79
Figure 4-27 Activate Stored Flight Plan Conﬁrmation ........... 79
Figure 4-28 Delete Flight Plan Conﬁrmation .......................... 80
Figure 4-29 Procedures Page................................................... 82
Figure 4-30 Selecting an Approach Procedure ....................... 84
Figure 4-31 Selecting an Approach Transition ........................ 84
Figure 4-32 Activating an Approach Procedure ...................... 85
Figure 4-33 Approach with No Procedure Turn ...................... 87

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

LIST OF FIGURES
Figure 4-34 Flying the Missed Approach ................................ 89
Figure 4-35 Flying the Procedure Turn .................................... 91
Figure 4-36 Flying the DME Arc and Vectors to the DME Arc 93
Figure 4-37 Flying a Holding Pattern ...................................... 95
Figure A-1 G1000 Alerting System .......................................... 97
Figure A-2 ADVISORY Softkey Annunciation ........................... 98
Figure A-3 G1000 System Failure Annunciations ................. 102

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

LIST OF TABLES

LIST OF TABLES
Table 3-1 Marker Beacon Signal Characteristics ...................41
Table 3-2 ICS Isolation Mode Transitions ..............................43
Table 3-3 ICS Operation Modes............................................44

viii

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

WARNINGS & CAUTIONS

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 Garmin G1000, as installed in Mooney M20M/R 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 altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could
vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer,
or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure
altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: The Jeppesen database used in the G1000 system must be updated regularly in order to ensure
that its information remains current. Updates are released every 28 days. A database information packet is
included in the G1000 package. Pilots using an outdated database do so entirely at their own risk.
WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non-navigational situational awareness. Any basemap indication should be compared with other navigation sources.
CAUTION: 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.
x

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

WARNINGS & CAUTIONS

CAUTION: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the G1000 Flight Manual Supplement. 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.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and
the pilot’s authority to operate this device under FAA/FCC regulations.
CAUTION: The GDU 1040 PFD and MFD displays use a lens coated with a special anti-reﬂective coating that
is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM
THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is speciﬁed as safe for anti-reﬂective coatings.
CAUTION: 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. Depictions of equipment may differ slightly from the actual equipment.
CAUTION: 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 Airman’s Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed as severe or giving an intense
radar echo.”
CAUTION: 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. Avoid the clusters to avoid the thunderstorms. In the cell display mode, even a single discharge point
may represent thunderstorm activity and should therefore be avoided.
WARNING: 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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

WARNINGS & CAUTIONS

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xii

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

SECTION 1: INTRODUCTION
Garmin® International Inc., a unit of Garmin Ltd.
introduces the G1000 Integrated Cockpit System for
the Mooney M20M and M20R aircraft. The G1000 includes the following Line Replaceable Units (LRUs):
•
•
•
•
•
•

GDU 1040 Primary Flight Display (PFD)
GDU 1040 Multi Function Display (MFD)
GIA 63 Integrated Avionics Units (2)
GEA 71 Engine/Airframe Unit
GDC 74A Air Data Computer (ADC)
GRS 77 Attitude & Heading Reference System
(AHRS)
• GMU 44 Magnetometer
• GMA 1347 Audio System with integrated Marker
Beacon Receiver
• GTX 32 Modes A/C or GTX 33 Mode S
Transponder

• G1000 Engine Indication System Pilot’s Guide
• G1000 GMA 1347 Audio Panel Pilot’s Guide and
Supplement
• G1000 VHF NAV/COM Pilot’s Guide
• G1000 Transponder Pilot’s Guide
• G1000 Annunciations & Alerts
• G1000 Pilot’s Guide Appendices
This Cockpit Reference Guide gives the pilot a basic
overview of the Primary Flight Display (PFD), Multi
Function Display (MFD), and the GMA 1347 Audio System.
NOTE: The pilot should read and thoroughly
understand the Mooney Aircraft Flight Manual
Supplement for limitations, procedures and
operational information not contained in this
Cockpit Reference Guide, The Mooney Aircraft
Flight Manual Supplement always takes precedence over the information found in this guide.

The purpose of this Cockpit Reference Guide is
to introduce the Mooney pilot to the major features
of the G1000 System. It is not intended to be a
comprehensive operating guide. Detailed in-depth
descriptions of the G1000 system are found in the
G1000 Pilot’s Guide documentation set. This documentation set contains the following:
• G1000 Multi Function Display Pilot’s Guide
• G1000 Primary Flight Display Pilot’s Guide

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

1.1 G1000 CONTROLS
1

Figure 1-1 G1000 Controls

NAV VOL/ID Control

Direct-to Key

NAV Frequency Toggle Key

Flight Plan Key

NAV Frequency Selector

Clear Key

Heading Selector

Flight Management System (FMS) knobs

Joystick

Menu Key

Course/Baro Selector

Procedures Key

COM Frequency Selector

Enter Key

COM Frequency Toggle Key

Altitude Reference Control

COM VOL/SQ Control

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION
The G1000 controls and keys have been designed to
simplify operations and minimize workload and time to
access sophisticated functionality. The following provides
an overview of the primary function(s) for each key and
control.
• (1) NAV VOL / ID Control – Controls the NAV
audio level. Press to toggle the ident ﬁlter ON and
OFF. Volume increase and decrease is shown in the
ﬁeld as a percentage.
• (2) NAV Frequency Toggle Key – Swaps the
standby NAV frequency and the active NAV frequency when pressed (the standby NAV frequency
is white whereas the active NAV frequency is green).
Note that NAV frequencies are shown as active only
when the HSI is set to either NAV1 or NAV2.
• (3) NAV Frequency Selector – The concentric
knobs tune the MHz (large) and kHz (small) standby
frequencies for the NAV receiver. Press on the small
knob to toggle the tuning cursor (cyan box) between
the NAV1 and NAV2 ﬁelds.
• (4) Heading Selector – Manually selects a heading.
When this knob is pressed, a window displaying a
digital heading momentarily appears to the left of the
Heading Indicator and the heading bug synchronizes
with the compass lubber line.
• (5) Joystick – Changes the map scale when rotated.
When pressed, it activates the map pointer.
• (6) CRS/BARO Selector – The large knob sets the
altimeter barometric pressure and the small knob
adjusts course. Course is adjustable when the HSI is
in NAV 1 & 2 or OBS/SUSP modes only). Pressing
the small knob centers the CDI on the currently
selected VOR.
• (7) COM Frequency Selector – The concentric
knobs tune the MHz (large) and kHz (small) standby
frequencies for the COM receiver. Pressing the
small knob toggles the tuning cursor (cyan box)

•

between the COM 1 and COM 2 ﬁelds.
(8) COM Frequency Toggle Key – Swaps the
standby COM frequency and the active COM frequency. Pressing and holding this key for ten seconds automatically makes the 121.5 MHz emergency
frequency the active frequency.
(9) COM VOL/SQ Control – Controls the COM
audio level. Pressing this knob turns the COM automatic squelch ON and OFF. Audio volume increase
and decrease is shown in the ﬁeld as a percentage.
(10) DIRECT-TO Key (
) – Allows the user to
enter a destination waypoint and establish a direct
course to the selected destination (speciﬁed by
identiﬁer, chosen from the active route, or taken
from the map cursor position).
(11) FPL Key – Displays the active Flight Plan
Page for creating and editing the active ﬂight plan
or accessing stored ﬂight plans.
(12) CLR Key (Default) – Erases information or
cancels an entry. To immediately display the Navigation Map Page, press and hold CLR (MFD only).
(13) FMS Knobs – The concentric knobs are
used to select the page to be viewed (only on the
MFD)— the large FMS knob selects a page group
(MAP, WPT, AUX, NRST) while the small FMS
knob selects a speciﬁc page within the page group.
Pressing the small FMS knob turns the on-screen
cursor ON and OFF. When the cursor is on, data
may be entered in the different windows using a
combination of the small and large FMS knobs.
The large FMS knob is used to move the cursor on
the page. The small FMS knob is used to select
individual characters for the highlighted cursor location. When the G1000 displays a list of information
that is too long for the display screen, a scroll bar
appears along the right side of the display. The scroll
bar graphically indicates the number of additional
items available within the selected category.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

•

Press the FMS/CSRS 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 options list allows the user to
access additional features or make settings changes
that relate to certain pages.
(15) PROC Key – Selects approaches, departures
and arrivals from the ﬂight plan. When using a
ﬂight plan, available procedures for 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. The procedures
key selects IFR departure procedures (DPs), arrival
procedures (STARs) and approaches (IAPs) from
the database and loads them into the active ﬂight
plan.
(16) ENT Key – Accepts a menu selection or data
entry. The enter key is used to approve an operation
or complete data entry. It is also used to conﬁrm
selections and information entries.
(17) Altitude Reference Control – Sets the reference altitude in the window over the altimeter tape.
The large ALT knob selects thousands, the small
ALT knob selects hundreds.

1.2 SECURE DIGITAL CARDS
The GDU 1040 data card slots use Secure Digital (SD)
cards. SD cards are used for aviation database updates
and terrain database storage.
To install an SD card:
1.

Press the card into place until it seats on the
internal connector and the front of the card is
ﬂush with the face of the display bezel

To remove an SD card:
1.

Gently press on the card to release the spring
latch and partially eject the card.
NOTE: Appendix A of the G1000 Pilot’s Guide
contains instructions on updating the aviation
database.

1.3 SYSTEM POWER-UP
The G1000 system is integrated with the aircraft electrical system and receives power directly from electrical
busses. See the Aircraft Flight Manual Supplement for
system start-up procedures.
Garmin G1000 PFD/MFD and supporting sub-systems include both power-on and continuous built-in test
features that exercise the processor, RAM, ROM, external
inputs and outputs to provide safe operation.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

PFD Power Up

MFD Power Up

As the G1000 system begins to initialize, test annunciations are displayed to the pilot on the PFD, as shown in
Figure 1-2. All system annunciations should clear within one minute of power up. The PFD also displays the
‘AHRS ALIGN: Keep Wings Level’ message. The AHRS
should display valid attitude and heading ﬁelds within 1
minute of power up. The AHRS can align itself while the
aircraft taxis or during level ﬂight.

The MFD Power-up Page displays general information
such as software version and database versions to the pilot
upon power-up of the G1000 system. The Power-up Page
displays the following data, shown in a scrolling list:
• System software version number.
• Copyright string.
• Checklist ﬁlename and copyright information.
• Land database name and version
• Terrain database information
• Obstacle database information
• Aviation database information (If the aviation database is out of date, then the pilot is forced to view
text that states the aviation database is out of date)
• Active Pilot Proﬁle

Figure 1-2 G1000 Power-Up

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

1.4 INITIAL OPERATIONS

1.6 REVERSIONARY MODE

The pilot may wish to change the active pilot proﬁle
(see the System Setup Section of the MFD Pilot’s Guide
for details).

In normal operating mode, the PFD displays graphical
ﬂight instrumentation in place of traditional gyro instruments. Attitude, heading, airspeed, altitude, and vertical
speed are all shown on one display. The MFD shows a
full-color moving map with navigation information. Both
displays offer control over COM and NAV frequency selectors, as well as heading, course/baro and altitude reference
functions. On the left of the MFD display, an Engine Indication System (EIS) cluster shows graphical depictions of
engine and airframe instrumentation. Figure 1-3 gives an
example of the G1000 system in normal mode.

When the Power-Up Page list has been reviewed for
currency (to ensure that no databases have expired), the
pilot is prompted to continue. The current database information (which is loaded in the system) is displayed
(valid operating dates, cycle number and database type
indicated).
Press the ENT key (or the right most softkey) to
acknowledge the list information and proceed to the Navigation Map Page. When the system has acquired a sufﬁcient number of satellites to determine a position, the
aircraft symbol appears showing your present position.

1.5 BACKLIGHTING
The G1000 PFD and MFD displays use photocell technology to automatically adjust for ambient lighting conditions. Photocell calibration curves are pre-conﬁgured
to optimize display appearance through a broad range of
cockpit lighting conditions. PFD, MFD, and GMA 1347
bezel/key lighting is normally controlled directly by the
existing instrument panel dimmer bus.
If desired, the PFD and MFD display backlights
may be adjusted manually. PFD, MFD, and GMA 1347
bezel/key brightness can also be adjusted manually as
well. GMA 1347 bezel/key brightness is directly tied to
the MFD bezel/key adjustment. Section 2 provides instructions on how to manually adjust the backlighting.

Should a failure occur in either display, the G1000 automatically enters reversionary mode. Figure 1-4 shows
an example where the PFD fails. In reversionary mode,
critical ﬂight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is also available on the reversionary mode
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 large red button on the bottom
of the GMA 1347. Pressing the red reversionary mode
button again deactivates reversionary mode.
NOTE: The system alerts the pilot when backup
paths are utilized by LRUs. Refer to the Annunciations & Alerts Pilot’s Guide for further information regarding these and other system alerts.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

Figure 1-3 G1000 Normal Mode

Figure 1-4 G1000 Reversionary Mode: Failed PFD

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

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Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

SECTION 2: PRIMARY FLIGHT
DISPLAY
This Cockpit Reference Guide describes the basic features of the Primary Flight Display (PFD) on the G1000
Integrated Cockpit System installed on Mooney aircraft.
The system consists of two 10.4 inch color ﬂat panel displays. During normal operation, the left display is conﬁgured as a Primary Flight Display. See the PFD Pilot’s
Guide for PFD descriptions and operating procedures not covered in this Cockpit Reference Guide.
The PFD provides increased situational awareness by
replacing the traditional “six pack” of instruments in the
pilot’s panel with a easy to scan display that provides a
large horizon, airspeed, attitude, altitude, vertical speed,
navigation, communication, annunciation, terrain, trafﬁc
and lightning information. The PFD will also control the
operation of the transponder, selecting NAV/COM frequencies and audio volume and many navigation features.
The operation of these features are explained in other supporting pilot’s guide documentation.
WARNING: In the event that the airspeed,
attitude, altitude or heading indications become
unusable please refer to the backup instruments.

The PFD displays the following:
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•

Navigation Frequency Window
Navigation Status Bar
Communication Frequency Window
Airspeed Indicator
True Airspeed Box
Attitude Indicator
Slip/Skid Indicator
Horizontal Situation Indicator
Bearing Pointers
Bearing Information Windows
Turn Rate Indicator
Altimeter
Altitude Reference Box
Barometric Setting Box
Vertical Deviation/Glideslope Indicator
Marker Beacon Receiver Annunciations
Vertical Speed Indicator
Alerts Window
Annunciation Window
System Time Box
Transponder Status Bar
Outside Air Temperature Box
Inset Map
Direct-to Window
Flight Plan Window
Procedures Window
Timer/References Window
Nearest Airports Window

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

13
2

9
8

Figure 2-1 Default PFD Information

NAV Frequency Window

Turn Rate Indicator

Airspeed Indicator

Barometric Setting Box

True Airspeed Box

Vertical Speed Indicator

Heading Box

Altimeter

Horizontal Situation Indicator

Altitude Reference Box

Outside Air Temperature Box

COM Frequency Window

System Time Box

Navigation Status Bar

Transponder Status Bar

Slip/Skid Indicator

Attitude Indicator

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

1
9

8
2

Figure 2-2 Additional PFD Information

Trafﬁc Annunciation

Alerts Window

Selected Heading Box

Selected Course Box

Inset Map

Annunciation Window

BRG1 Information Window

Vertical Deviation/Glideslope Indicator

BRG2 Information Window

Marker Beacon Annunciation

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

2.1 BACKLIGHTING
The backlighting of the display and the keys can be
adjusted for the PFD and MFD. The backlighting intensity ranges from 0.14% to 100.00%. Two modes exist for
adjustment:
• Auto - The G1000 adjusts the backlighting automatically with reference to the amount of light in
the cockpit (default setting).
• Manual - Allows the pilot to manually adjust the
backlighting.
NOTE: Except in reversionary mode, the backlighting can only be adjusted from the PFD.
NOTE: No other window can be displayed in the
lower right corner of the PFD when the MENU
key is pressed to change the backlighting.

To manually adjust the backlight for the
PFD and MFD:

Press the MENU key on the PFD to display
the PFD Setup Menu window. ‘AUTO’ is now
highlighted next to ‘PFD DSPL’.

Turn the small FMS knob to display the selection window. Turn the FMS knob to select
‘MANUAL’, then press the ENT key.

With the intensity value now highlighted,
turn the small FMS knob to select the desired
backlighting, then press the ENT key.

Turn the large FMS knob to highlight ‘AUTO’ next
to ‘MFD DSPL’ and repeat steps 2 and 3. Press
the CLR or MENU key to remove the window.

To manually adjust the backlight for the
PFD and MFD keys:
1.

Press the MENU key on the PFD to display
the PFD Setup Menu Window. ‘AUTO’ is now
highlighted next to PFD DSPL.

Turn the large FMS knob to highlight PFD DSPL.
Turn the small FMS knob in the direction of the
green arrow to display PFD KEY.

Turn the large FMS knob to highlight ‘AUTO’.
Turn the small FMS knob to display the selection window. Turn the FMS knob to select
‘MANUAL’, then press the ENT key.

With the intensity value now highlighted,
turn the small FMS knob to select the desired
backlighting, then press the ENT key.

Turn the large FMS knob to highlight MFD DSPL
and turn the small FMS knob in the direction of
the green arrow to display MFD KEY. Repeat
steps 3 and 4. Press the CLR or MENU key to
remove the window.

Figure 2-3 PFD Setup Menu

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

2.2 SOFTKEY FUNCTION
When a softkey is turned on, its color changes to black
text on gray background and remains this way until it is
turned off, at that time it changes to white text on black
background. The CDI, IDENT, TMR/REF, NRST and
ALERTS softkeys change momentarily to black text on
gray background and automatically switches back to
white text on black background.
Softkey On

Softkey Off

The PFD softkeys listed provide control over ﬂight
management functions including GPS, NAV, terrain, trafﬁc and lightning.
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
TRAFFIC – Press to display TIS trafﬁc on the
map.
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.
LTNG – Press to display the lightning data on
the inset map (within a 200 nm radius of the
aircraft).
BACK – Press to return to the previous level
softkey conﬁguration.

PFD – Press to display the additional softkeys for
additional conﬁgurations to the PFD.
METRIC – Press to display the current and reference altitudes in meters, in addition to feet.
Pressing the metric softkey also changes the
barometric setting to hectopascals.
DFLTS – Press to reset default settings on the PFD.
BRG1 – Press to display the BRG (bearing) 1 information window.
OFF – Press to remove BRG1 information
window.
NAV1 – Press to display NAV1 waypoint
frequency or identiﬁer and DME information
in the BRG1 information window.
GPS – Press to display GPS waypoint identiﬁer
and DME information in the BRG1 information
window.
BACK – Press to return to the previous level
softkeys.
360 HSI – Press to display the 360° compass rose.
ARC HSI – Press to display the 140° viewable arcs.
BRG2 – Press to display the BRG (bearing) 2 information window.
NAV2 – Press to display NAV2 waypoint
frequency or identiﬁer and DME information in
the BRG2 information window.
OFF – Press to remove the BRG2 information
window.
BACK – Press to return to the previous level
softkeys.
STD BARO – Press to set the barometric pressure
to 29.92 inches of mercury (1013 hPa by
pressing the METRIC softkey).
BACK – Press to return to the previous level softkeys.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

INSET

DCLTR

OFF

DCLTR-1

TRAFFIC

TERRAIN

TOPO

BACK

ALERTS

Press The BACK or OFF Softkey
To Return To The Top Level
Softkeys

DCLTR-2

DCLTR-3

PFD

Press the BACK softkey to return
to the top level softkeys
METRIC

DFLTS

360 HSI

ARC HSI

STD BARO

BACK

Press the DFLTS softkey to change the PFD
metric values to standard

Figure 2-4 PFD Softkeys (1 of 2)
14

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

ALERTS

SECTION 2 – PFD

CDI

XPDR

OBS

TMR/REF

IDENT

NRST

ALERTS

CDI (NAV1)

Press the BACK softkey
to return to the top level
softkeys

CDI (NAV2)

ALT

STBY

VFR

CODE

IDENT

BACK

ALERTS

Press the BACK
softkey
to return to
the top level
softkeys
0

IDENT

BKSP

BACK

ALERTS

Figure 2-4 PFD Softkeys (2 of 2)

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
CDI – Press to change navigation mode on the CDI
between GPS NAV1 and NAV2.
OBS – Press to select OBS mode on the CDI when
navigating by GPS.
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 mode.
VFR – Press to automatically squawk 1200 (only
in the U.S.A.).
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.

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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

2.3 FLIGHT INSTRUMENTS
Airspeed Indicator
The Airspeed indicator displays airspeed on a rolling
number gauge using a moving tape. The following information is also displayed:
•
•
•
•

Speed Ranges
A color coded (white, green, yellow, and red) speed
range strip is located on the moving tape. The colors denote ﬂaps operating range, normal operating range, caution range, and never exceed speed (Vne). A red range is
also present for low speed awareness. Refer to the Aircraft
Flight Manual Supplement (AFMS) for speed criteria.

Speed indication
Speed ranges
Airspeed trend vector
Vspeed references

Airspeed Trend
Vector

Vspeed
References

Actual Airspeed

Speed Ranges

True Airspeed
Box
Figure 2-5 Airspeed Indicator

Speed Indication
The numeric labels and major tick marks on the moving tape are marked at intervals of 10 knots, while minor
tick marks on the moving tape are indicated at intervals
of 5 knots. Speed indication starts at 20 knots, with 60
knots of airspeed viewable at one time. The actual airspeed is displayed inside the black pointer. The pointer
remains black until reaching never exceed speed (Vne), at
which point it turns red.

Figure 2-6 Red Pointer at Vne

Airspeed Trend Vector
The vertical, magenta line extends up or down on the
airspeed scale located left of the numeric labels. The end
of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration is maintained. The trend vector is absent if the speed
remains constant and if any data needed to calculate airspeed is not available due to a system failure.
Vspeed References
Vspeeds are set using the TMR/REF softkey. Vr, Vx, Vy
and Glide are shown on the References window. When
active (ON), the Vspeeds are displayed at their respective
locations to the right of the airspeed scale (refer to the
Auxiliary windows section in this Pilot’s Guide to set and
display Vspeeds).
True Airspeed Box
The True Airspeed box is located below the Airspeed
indicator and displays the true airspeed in knots.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

Attitude Indicator

Pitch Indication

The attitude information displays over a virtual blue
sky and brown ground with a white horizon line. The
aircraft wing tips are represented by two yellow bars on
the horizon line. The yellow inverted “V” represents the
aircraft. The Attitude indicator displays the following information:
• Pitch indication
• Roll indication
• Slip/Skid indication

Major pitch marks and numeric labels at 10, 20, 30,
40, 50, 60, 70 and 80 degrees are shown above and below the horizon line. Minor pitch marks at 5, 15 and 25
degrees above the horizon line and 5, 15, 25, 35 and 45
degrees below the horizon line are shown. The horizon
line is part of the pitch scale. Red extreme pitch warning
chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon
line (refer to the ﬁgures on the next page).

7
3
6
4
5

Figure 2-7 Attitude Indicator

Roll Pointer

Roll Scale

Horizon Line

Aircraft Symbol

Land Representation

Aircraft Wing Tips

Pitch Scale

Slip/Skid Indicator

Sky Representation

Roll Index

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
Roll Indication
Major tick marks at 30 and 60 degrees and minor tick
marks at 10, 20 and 45 degrees are shown to the left and
right on the roll scale. The inverted white triangle indicates 0 on the roll scale. Angle of bank is indicated by the
position of the roll pointer on the roll scale.
NOTE: Supplemental ﬂight data such as the Inset
Map, Alerts and Annunciation Window disappear
from the PFD when pitch is more than +30˚
and less than -20˚ or when a 65˚ bank angle is
reached.
Figure 2-8 Attitude Indicator Nose High

Slip/Skid Indication
The Slip/Skid indicator resides beneath the roll pointer.
The indicator moves with the roll pointer and moves laterally away from the pointer to indicate lateral acceleration.
A slip/skid is indicated by the location of the Slip/Skid indicator relative to the roll pointer. One Slip/Skid indicator
displacement is equal to one ball displacement when compared to a traditional Slip/Skid indicator.

Figure 2-9 Attitude Indicator Nose Low

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

Altimeter

Altitude Reference Bug

The Altimeter displays barometric altitude values in
feet on a rolling number gauge using a moving tape. The
Altimeter displays the following information:
•
•
•
•
•
•
•

The Altitude Reference Bug is displayed at the reference
altitude or the edge of the tape (whichever is closer to the
current altitude) to provide increased altitude awareness.
Altitude Trend Vector

Altitude values
Altitude reference bug
Altitude trend vector
Altitude reference box
Barometric setting box
Altitude alerter
Metric display
Altitude Reference
Box

Altitude Reference Bug
Altitude Trend
Vector

The vertical, magenta line extends up or down the altitude scale located right of the numeric labels. The end of
the trend vector displays approximately what the altitude
will be in 6 seconds if the current rate of vertical speed is
maintained. The trend vector is absent if altitude remains
constant or if any data needed to calculate it is not available due to a system failure.
Altitude Reference Box
The Altitude Reference box displays the reference altitude in feet. The metric value, when selected, is displayed
on top the Altitude Reference box.
Barometric Setting Box

Current Altitude

The Barometric Setting Box displays the barometric
pressure in inches of mercury (in Hg) or hectopascals
(hPa).
To select barometric pressure:
1.

Barometric Setting
Box

Turn the large BARO (outer) knob to select
the desired setting.

Figure 2-10 Altimeter

Altitude Values
The numeric labels and major tick marks are shown
at intervals of 100 feet. Minor tick marks are at intervals
of 20 feet. The current altitude is displayed in the black
pointer.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
Altitude Alerting
Altitude alerting provides the pilot with a visual and
aural alert when approaching the reference altitude.
Although ﬂight control systems use the same reference
altitude box the altitude alerter does, the altitude alerter
is not coupled to a ﬂight control system and can function without one. The visual annunciations appear in the
altitude reference box. Anytime the reference altitude is
changed, the altitude alerter is reset.
There is an altitude band set at +/- 1,000 ft. of the reference altitude and a deviation band set at +/- 200 ft. of
the reference altitude. When the pilot climbs or descends
to the reference altitude an aural alert (single tone) sounds
and the reference altitude ﬂashes (cyan on black) for 5
seconds then changes to black on cyan as the aircraft passes through +/- 1,000 ft. of the reference altitude.
When the aircraft passes within +/- 200 ft. of the reference altitude, the reference altitude ﬂashes (cyan on
black) again indicating that the aircraft is within the deviation band. Each time the pilot ﬂies outside the deviation
band (+/- 200 ft. of the reference altitude), an aural alert
is generated and the reference altitude ﬂashes (yellow on
black) for 5 seconds.

Figure 2-12 Altimeter within 1,000 ft. of Reference Altitude

Figure 2-11 Colors Associated with the Altitude Alerter

Figure 2-13 Altimeter within 200 ft. of Reference Altitude

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
Metric Display
Reference and current altitude can be displayed in meters. The barometric pressure may also be displayed in
hectopascals.
To display altitude in meters and barometric
pressure in hectopascals:
1.
2.

Press the PFD softkey to display the second
level softkeys.
Press the METRIC softkey to display altitude in
meters and barometric pressure in hectopascals.
Press the BACK softkey to return to the top level
softkeys.

Vertical Deviation/Glideslope Indicator
The Vertical Deviation/Glideslope Indicator is a window on the left side of the Altimeter. The window appears
when an ILS is tuned in the active NAV ﬁeld (and selected
on the Audio Panel). A green diamond appears and acts
as your vertical deviation indication, just like a glideslope
needle on a conventional indicator.

Marker Beacon Annunciations
Marker Beacon Annunciations are displayed on the
PFD to the left of the Altitude Reference Box. Outer marker reception is indicated by a blue light. Middle marker
reception is indicated by a amber light. Inner marker reception is indicated by a white light (refer to the Audio
Panel Pilot’s Guide for more information).
Marker Beacon
Annunciation

Vertical
Deviation/Glideslope
Indicator

Figure 2-14 Altimeter (Metric)

Figure 2-16 Marker Beacon and Vertical Deviation

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

Vertical Speed Indicator
The Vertical Speed Indicator displays the aircraft vertical speed with numeric labels and tick marks at 1,000 ft.
and 2,000 ft. in each direction on the non-moving tape.
Minor tick marks are at intervals of 500 ft.
Vertical Speed Pointer
The Vertical Speed Pointer displays the current vertical
speed and points to that speed on the non-moving tape. If
the rate of ascent is greater than 2,000 feet per minute the
pointer will appear at the top edge of the non-moving tape
and the number of feet per minute will appear inside the
pointer. If the rate of descent is greater than 2,000 feet per
minute a negative sign is displayed in the pointer (-2,000)
for negative (down) vertical speed and the pointer will appear at the bottom edge of the non-moving tape.
NOTE: Digits appear in the pointer when the
climb or descent rate is >100 fpm.

Vertical Speed
Pointer

Figure 2-16 Vertical Speed Indicator

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

Horizontal Situation Indicator
The Horizontal Situation Indicator (HSI) displays a rotating compass card with letters at the cardinal points and
numeric labels every 30 degrees. Major tick marks are
at 10 degree intervals and minor tick marks for every 5
degrees. The HSI is displayed in a heading up orientation.
The HSI compass can be displayed as a 360° rose or 140°
arc by pressing the PFD softkey, followed by the 360 HSI
or the ARC HSI softkey. The HSI displays the following
information:
•
•
•
•
•
•

Heading indication
Turn Rate indicator
Course Deviation Indicator
Bearing pointers
Bearing information windows
Navigation source

9
8

Figure 2-18 Horizontal Situation Indicator
1
2
3
4
5
6
7

Lateral Deviation
Scale

Course Deviation and
TO/FROM Indicator

Figure 2-17 ARC HSI

8
9
10
11
12
13
14

Turn Rate Indicator
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

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
Heading Indication

Course Deviation Indicator

A digital reading of the current magnetic heading appears on top of the HSI. A rotatable heading bug on the
compass rose and arc marks the desired heading. When
the pilot selects a heading, a digital reading will appear for 3
seconds in a box left of the lubber line, next to the HSI.

Figure 2-19 Selected Heading Box

The HSI contains a course deviation indicator (CDI),
with a course pointer arrow, TO/FROM arrow, a sliding
deviation bar and scale. The course pointer is a single
line arrow (GPS and NAV1) or double line arrow (NAV2),
which points in the direction of the set course. The TO/
FROM arrow rotates with the course pointer and is displayed when the active navaid is received. The sliding
deviation bar moves left or right from the course pointer
along a scale to display aircraft position relative to the
course. When the pilot selects a course, a digital reading
will appear for 3 seconds in a box right of the lubber line,
next to the HSI.

NOTE: The heading displayed on the HSI is always
magnetic, even if the NAV ANGLE is set to ‘TRUE’
in the AUX System Setup Page on the MFD.

Turn Rate Indicator
The Turn Rate Indicator resides directly above the rotating compass card. Each tick mark is at 9 (half standard
rate) and 18 (standard rate) degrees to the left and right of
the lubber line. A wide magenta line displays the current
turn rate up to 24 degrees. A magenta arrowhead appears
at 25 degrees and disappears at 24 degrees. This trend
vector provides the pilot with a 6 second prediction of
what the heading will be at the present turn rate.

Figure 2-21 Selected Course Box

The CDI has angular limits exactly the same as a mechanical CDI when coupled to a VOR or LOC. When
coupled to GPS, the full scale limits for the CDI are deﬁned by a GPS derived distance (5.0, 1.0 or 0.3 nm). The
CDI scale automatically adjusts to the desired limits based
upon the current phase of ﬂight (enroute 5.0 nm, terminal
area 1.0 nm or approach 0.3 nm). The desired GPS scale
settings may be selected manually from the MFD (refer to
the MFD Pilot’s Guide).

Figure 2-20 Turn Rate Indicator and Trend Vector

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
Bearing Pointers and Information Windows
There are 2 bearing pointers available, 1 or 2 can be
displayed on the HSI. Pressing the PFD softkey provides
access to the BRG1 and BRG2 softkeys. BRG1 pointer is
a single cyan (light blue) line with an open arrowhead at
the end. BRG2 pointer is a double cyan (light blue) line
with an open arrowhead at the end. The bearing pointers never override the CDI. When one or more bearing
pointers are displayed (but not necessarily visible if there
is no data available), a white ring is presented around the
center of the compass rose to visually separate the bearing
pointer(s) from the CDI.
When a bearing pointer is displayed it’s associated
information window is also displayed. BRG1 information window is displayed to the lower left of the HSI
and includes the bearing source (NAV1), a pointer icon,
frequency and distance (NAV1 and GPS) to the bearing
source. BRG2 information window is displayed to the
lower right of the HSI and includes the bearing source
(NAV2), a pointer icon, frequency and distance (NAV2) to
the bearing source.
If GPS is the bearing source, the active waypoint identiﬁer is displayed in lieu of a frequency. If an active waypoint is not selected, the bearing pointer is removed from
the HSI and “NO DATA” is displayed in the information
window.
If the NAV radio is the bearing source and is tuned to
an ILS frequency, the bearing pointer is removed from the
HSI and the frequency is replaced with “ILS”. If the NAV
radio is not receiving the tuned VOR station, the bearing
pointer is removed from the HSI and the frequency displayed in the information window is replaced with “NO
DATA”.
When NAV1 or NAV2 is the selected bearing source,
the frequency is replaced by the station identiﬁer when
the station is in range.

Bearing 1
Pointer

Bearing 2
Pointer

Bearing 1
Information
Window

Bearing 2
Information
Window

Figure 2-22 HSI with Bearing Information
Distance from
Waypoint
Waypoint
Identiﬁer
Bearing
Source

Pointer
Icon

Figure 2-23 BRG1 Information Window
Distance from
Waypoint
Waypoint
Identiﬁer
Pointer
Icon

Bearing
Source

Figure 2-24 BRG2 Information Window

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD
Navigation Source
The HSI can display two sources of navigation, GPS
or NAV (VOR, localizer, and glideslope). In GPS mode
the ﬂight plan legs are sequenced automatically. Enabling
OBS mode suspends auto sequencing of waypoints, but
retains the current “active to” waypoint as your navigation
reference even after passing the waypoint. When OBS is
disabled the GPS returns to normal operation, with automatic sequencing of waypoints. OBS mode also allows
the pilot to set the desired course TO/FROM a waypoint.

To enable/disable OBS mode while navigating
with GPS:
1.

Press the OBS softkey to select OBS Mode.

Turn the small CRS knob to select the desired
course TO/FROM the waypoint.

Press the OBS softkey again to return to normal
operation.

Color indicates the current navigation source, magenta
(for GPS ) or green (for NAV). As the user crosses the
MAP, “SUSP” appears on the HSI in place of OBS and the
OBS softkey now reads “SUSP”, indicating that automatic
sequencing of approach waypoints is suspended at the
MAP. A yellow ‘INTEG’ and ‘WARN’ may appear on the
HSI when the following occurs:
• INTEG – RAIM is not available
• WARN – GPS detects a position error
To change between navigation sources:
1.

Press the CDI softkey to change from GPS to
NAV1. This will place the cyan tuning box over
the NAV1 standby frequency in the upper left
corner of the PFD.
Press the CDI softkey again to change from
NAV1 to NAV2. This will place the cyan tuning
box over the NAV2 standby frequency.
Press the CDI softkey a third time to return to
GPS.

Figure 2-25 GPS INTEG, GPS SUSP, NAV1 and NAV2

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

2.4 COMMUNICATION, NAVIGATION &
SURVEILLANCE
Communication Frequency Window
The Communication Frequency window provides the
control and display of dual VHF Radio Communication
Transceivers (COM1 and COM2). The Communication
Frequency window displays the following information:
• COM1 and COM2 active and standby frequencies
• Color coded indication of the active COM transceiver
NOTE: Operating procedures for the Communication Frequency window are located in the VHF
NAV/COM Pilot’s Guide.

Active COM
Frequency Field

Frequency
Tuning Box

Selected COM
Frequency
(Green)

COM Radios
Frequency
Toggle Arrow

Standby COM
Frequency Field

Figure 2-26 Communication Frequency Window

Navigation Frequency Window
The Navigation Frequency window provides the control and display of dual VOR/ILS receivers (NAV1 and
NAV2). The Navigation Frequency window displays the
following information:
• NAV1 and NAV2 active and standby frequencies
• NAV1 and NAV2 identiﬁer, if the active NAV1 or
NAV2 frequency is a valid, identiﬁed frequency
• Color coded indication of the active NAV receiver
NOTE: Operating procedures for the Navigation Frequency window are located in the VHF NAV/COM
Pilot’s Guide.

Frequency
Tuning Box

Active NAV
Frequency Field
Selected NAV
Frequency
(Green)

NAV Receivers
Standby NAV
Frequency Field

Frequency
Toggle Arrow

Figure 2-27 Navigation Frequency Window

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

Navigation Status Bar
The Navigation Status Bar resides at the top of the PFD
and displays valuable information while ﬂying a route.
The following information is displayed:
•
•
•
•
•

The next waypoint in the active ﬂight plan
Distance to the next waypoint (DIS)
Desired track to the next waypoint (DTK)
Current track angle (TRK)
GPS Navigation Annunciations
NOTE: The ﬁelds in the PFD Navigation Status
Bar cannot be changed.

Next Waypoint

Distance to
Next Waypoint

Desired Track
To
Next Waypoint

Current Track

Figure 2-28 Navigation Status Bars

Figure 2-29 Navigation Status Bar Message

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

Transponder Status Bar
The Transponder Status Bar displays the transponder
code, reply symbol, and mode of operation. TIS (Trafﬁc
Information System) surveillance data up-linked by Air
Trafﬁc Control (ATC) radar through the GTX33 Mode S
Transponder appears on the Inset Map (PFD), Navigation
and Trafﬁc Map Pages on the MFD (refer to the MFD Pilot’s
Guide). If the transponder is conﬁgured with Automated
Airborne Determination, normal operation begins when
lift off is sensed. When the aircraft is on the ground, the
window automatically displays “GND”. The transponder
does not respond to ATCRBS interrogations when GND is
annunciated. If a delay time is set in Conﬁguration Mode,
the transponder waits a speciﬁed length of time after landing before changing to GND mode.
Transponder Operation
Pressing the XPDR softkey displays the second-level
softkeys:
• STBY – Selects standby mode. When in standby
mode, the transponder does not reply to any
interrogations.
• ON – Selects Mode A. In this mode, the transponder replies to interrogations, as indicated by the
Reply Symbol (R). Replies do not include altitude
information.
• ALT – Selects Mode C. In ALT mode, the transponder replies to identiﬁcation and altitude
interrogations as indicated by the Reply Symbol
(R). Replies to altitude interrogations include the
standard pressure altitude received from an external altitude source, which is not adjusted for barometric pressure. The ALT mode may be selected
in aircraft not equipped with an optional altitude
encoder; however, the reply signal will only reply
to mode A interrogations. The transponder also
responds to interrogations from TCAS equipped
aircraft.
• VFR – Sets the transponder code to the pre-pro30

grammed VFR code selected in Conﬁguration
Mode (this is set to 1200 at the factory).
• CODE – Displays the transponder code selection
softkeys, which includes the digits 0-7 and BKSP.
• IDENT – Pressing the IDENT softkey activates
the Special Position Identiﬁcation (SPI) Pulse for
18 seconds, identifying the transponder return on
the ATC screen.
Transponder Code Selection
Transponder code selection is performed with eight
softkeys (0-7) providing 4,096 active identiﬁcation codes.
Pushing one of those keys begins the code selection sequence. The new code is activated ﬁve seconds after the
fourth digit is entered. Pressing the BKSP softkey removes
one digit at a time until the status bar is empty (refer to the
Mode S Transponder Pilot’s Guide).

Figure 2-30 Transponder Status Bar

2.5 ALERTS AND ANNUNCIATIONS
Alerts and Annunciations that appear on the PFD are
described in detail in Appendix A of this Cockpit Reference Guide.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

SECTION 3: AUDIO PANEL
The GMA 1347 Audio Panel features the following
three (3) major groups of keys in descending order, as
shown in Figure 3-1:
• Communication keys
• Navigation keys
• Intercom keys
Each key is labeled with a white inscription in its center, indicating the name of the associated channel. The
triangular key annunciator lights are white when illuminated and point to the corresponding keys.
The dual knob located at the bottom of the unit controls volume as well as squelch threshold levels. The
small knob adjusts the volume/squelch level associated
with the pilot channel, while the large knob adjusts the
volume/squelch level associated with the copilot/passenger channels. The red button situated below the dual volume/squelch knob controls backup (reversionary) mode
selection.
NOTE: A complete audio panel description with
full operating procedures is presented in the
G1000 Audio Panel Pilot’s Guide.
NOTE: Refer to the Audio Panel Pilot’s
Guide Supplement for Mooney for additional information regarding the
GMA 1347 as installed in Mooney aircraft.

3.1 FRONT PANEL CONTROLS
• Transceiver audio selector keys
(COM1, COM2, COM3)
• Transmitter (audio/mic) selection keys
(COM1 MIC, COM2 MIC, COM3 MIC)
• Split COM key
(COM 1/2)
• Dedicated telephone interface key
(TEL)
• Passenger address key
(PA)
• Speaker key
(SPKR)
• Marker beacon receiver audio select/mute key
(MKR/MUTE)
• Marker beacon receiver high sensitivity key
(HI SENS)
• Aircraft radio audio selector keys
(NAV1, NAV2, ADF, DME, AUX)
• Intercom manual squelch mode key
(MAN SQ)
• Digital recording playback key
(PLAY)
• Intercom system (ICS) isolation mode keys
(PILOT, COPLT)
• Volume/squelch knob
(VOL/SQ)
• Backup (reversionary) mode button
(DISPLAY BACKUP)

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

Transceiver Audio

Transmitters

Telephone

Split COM
Passenger Address

Speaker
Marker Beacon Signal Sensitivity

Marker Beacon/Mute

Aircraft Navigation Radio Audio
Aircraft Navigation Radio Audio

Manual Squelch

Digital Recording Playback
ICS Isolation

VOL/SQ
VOL Annunciation

SQ Annunciation
Reversionary Mode

Figure 3-1 Front Panel Controls

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

Microphones
The GMA 1347 features six (6) different microphone
channeling modes:

•
•
•
•
•
•

COM1 MIC
COM2 MIC
COM3 MIC
COM 1/2 (Split COM)
PA
COM 1/2 and PA (Split COM and PA)
NOTE: A push-to-talk (PTT) switch must be
pressed to open the selected output channel.

Each audio panel can accept up to six (6) microphone
inputs, thus allowing for a two-person crew and up to
four (4) passenger intercom stations in the aircraft.

In Conﬁguration mode, headset audio level can be adjusted above or below a nominal value for MUSIC 1, MUSIC
2, UNSWITCHED 1, UNSWITCHED 2, UNSWITCHED
3 and ALTITUDE WARNING. Please consult a Garminauthorized service center for additional information.

Unmuted/Unswitched Inputs
The unit provides four (4) unmuted/unswitched inputs that are always presented to the headsets or speakers
connected to the panel. These inputs are the following
aural warnings:

•
•
•
•

ALT warning
UNSWITCHED 1
UNSWITCHED 2
UNSWITCHED 3

Mono/Stereo Headsets
The GMA 1347 can accommodate up to six (6) headsets (pilot, copilot and up to four (4) passengers).
NOTE: The use of stereo headsets is highly
recommended. However, if monaural headsets
are plugged into stereo jacks that do not each
have a switch installed, the unit will not be damaged.

Use of a monaural headset in a stereo jack shorts the
right headset channel output to ground. Thus, a person
listening on a monaural headset only hears the left channel in both ears. If a monaural headset is used at one of
the passenger positions, any other passenger listening on
a stereo headset hears audio in the left ear only, unless the
headset has a mono/stereo switch and the latter is set to
mono.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

3.2 UNIT OPERATION
Power-up Settings
Upon power-up, the unit undergoes a self-test during
which all panel annunciator lights illuminate for approximately two (2) seconds. Once the self-test is completed,
the settings are restored to the settings that were current
before the unit was last powered off. For example, if the
COM1 MIC, COM1, COM2, SPKR, NAV1, NAV2,
MKR/MUTE, HI SENS, and MAN SQ keys were selected
when the unit was last powered off, these keys will be
automatically re-selected when the unit is powered back
on.

Fail-safe Mode
In the event of an audio panel failure, the unit switches
to fail-safe mode. In fail-safe mode, fail-safe audio is directed to the pilot’s headset (left channel only). Fail-safe
mode bypasses the GMA 1347 circuits, with the exception
of the relay that switches the pilot’s MIC and the pilot’s
headset directly to COM1.

Selecting Keys
For all keys with the exception of the MKR/MUTE
and PLAY keys, pressing a key activates the corresponding channel and illuminates the associated triangular annunciator light.

Deselecting Keys
For all keys with the exception of the COM MIC,
MKR/MUTE and PLAY keys, pressing the key again deactivates the corresponding channel and turns off the associated annunciator light.
NOTE: Operational details on the COM MIC,
MKR/MUTE and PLAY keys as well as the DISPLAY BACKUP button are provided later in this
manual.

Lighting
LED key backlighting is controlled automatically by
the MFD (the PFD assumes control should the MFD fail).
NOTE: When a key is active during normal operations, its corresponding annunciator LED is lit.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

Transceiver Keys

Pressing a COM Key

As illustrated below, the following eight (8) transceiver keys appear at the top of the GMA 1347 front panel:
COM1 MIC, COM2 MIC, COM3 MIC, COM 1/2,
COM1, COM2, COM3, and TEL. COM audio can be
selected by either pressing the desired COM key or by
pressing the corresponding COM MIC key.

Pressing COM1, COM2, or COM3 selects the corresponding radio as the active audio source. Each audio
source can be selected independently by pressing COM1,
COM2, or COM3. If selected in this manner, the audio source remains selected independently of the active
microphone source selection. The active COM audio is
always heard through the headsets, and any combination
of audio sources can be selected simultaneously.

NOTE: A PTT switch must be pressed to allow
all microphone transmissions.

During COM signal reception, a white RX inscription appears next to the corresponding COM frequency
on both the PFD and the MFD for the duration of the
reception.

Keying a Microphone
When a microphone is keyed, the active transceiver
MIC key annunciator blinks approximately once per second to indicate that the transmission is active, and a white
TX inscription appears next to the corresponding COM
frequency on both the PFD and the MFD for the duration
of the transmission.
Figure 3-2 Transceivers

Pressing a COM MIC Key
Pressing COM1 MIC, COM2 MIC, or COM3 MIC
selects the corresponding radio as the active microphone
source (i.e., as the primary COM radio) and highlights
the corresponding COM frequency in green in the active
frequency ﬁeld of the PFD and MFD.
Only one microphone source can be selected at a time.
Thus, if COM1 MIC is pressed when COM2 MIC is already selected, COM2 MIC is automatically deactivated
and the COM2 MIC annunciator light is turned off. The
corresponding audio selection key (in this case, COM1)
becomes automatically selected if it is not already selected
at the time.

When no further aircraft radio activity is detected by
the unit, the amount of ambient background noise from
the radios is further reduced by the MASQTM (Master Avionics Squelch) circuit (information on MASQTM is presented later in this manual).
NOTE: Audio level of the selected COM radio(s)
is controlled by the COM radio volume control
located on both the PFD and MFD (see G1000
VHF NAV/COM Pilot’s Guide for more information).

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

COM Swap
The GMA 1347 allows for the use of a remotely mounted switch to alternately transfer the active microphone
between COM1 MIC and COM2 MIC. The COM swap
switch is typically mounted on the yoke or control stick.
If COM1 MIC is the active microphone (i.e., both COM1
MIC and COM1 keys are annunciated), pressing the COM
swap switch transfers the active microphone from COM1
MIC to COM2 MIC (i.e., both COM1 MIC and COM1
keys become deselected, and COM2 MIC and COM2
keys become annunciated). Pressing the switch has no effect if COM3 is the active transceiver or if COM 1/2 (split
COM) is activated.
Please consult a Garmin-authorized service center for
details on the remote COM swap option.

Split COM

NOTE: Split COM performance varies signiﬁcantly
across installations and is affected by both the
distance between the antennas and the separation of the tuned frequencies. In small aircraft
particularly, receiver sensitivity is typically
reduced and squelch breaks are affected. Each
installation should be individually examined to
determine the expected performance of split
COM.

PA Function
The passenger address function is provided via the PA
key. Push-to-talk (PTT) must be used to deliver PA announcements.
NOTE: PA volume is adjustable in Conﬁguration
mode.

Pressing the COM 1/2 key toggles the state of the split
COM function. During split COM operation, the COM1,
COM1 MIC, COM2 and COM2 MIC keys are annunciated and thus active.
When the COM 1/2 key is selected, COM1 becomes
dedicated solely to the pilot for MIC/audio, while COM2
becomes dedicated to the copilot for MIC/audio. The
COM1 MIC annunciator blinks when the pilot’s microphone is keyed. The COM2 MIC annunciator blinks
when the copilot’s microphone is keyed.
In this mode, both the pilot and the copilot can
simultaneously transmit over separate radios. Note that,
while the pilot can still monitor COM3, NAV1, NAV2,
DME, ADF, AUX and MKR audio as selected, the copilot is
only able to monitor/hear COM2.
Split COM mode is cancelled by pressing the COM 1/2
key.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

Split COM and PA

Speaker Output

When in split COM mode (COM 1/2 activated), the
copilot can make PA announcements while the pilot continues to use COM1 independently. When the PA key is
pressed after the split COM mode is activated, the copilot’s
microphone is output over the cabin speaker when keyed.
Pressing the PA key again returns the copilot to normal
split COM operation.

Pressing the SPKR key selects the aircraft radios to be
output to the cabin speaker. Pressing the SPKR key again
deselects the speaker mode. When SPKR is selected, any
and all of the following radios can be heard over the cabin
speaker: COM1, COM2, COM3, NAV1, NAV2, DME,
ADF, and AUX.

NOTE: Only the copilot can make PA announcements when in split COM and PA mode.

Speaker output is muted when the PTT switch is
keyed. All of the unswitched/unmuted radio inputs can
be heard over the speaker. In Conﬁguration mode, speaker audio level is adjustable above and below a nominal
value. Please consult a Garmin-authorized service center
for details.

Figure 3-3 Split COM, PA and Speaker

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

3.3 MARKER BEACON RECEIVER
Description and Operation
The GMA 1347 provides a marker beacon receiver to
be used as part of an ILS approach. In addition to the
normal marker beacon receiver functions, the GMA 1347
provides an audio muting capability. The marker beacon receiver is always “ON” and receives at 75 MHz.
The receiver detects three (3) tones associated with the
outer, middle and inner approach markers, respectively,
and illuminates the appropriate marker beacon indicator lights located to the left of the Altimeter on the PFD.
The outer marker signal frequency is 400 Hz, and a blue
light indicates its reception. The middle marker signal
frequency is 1,300 Hz, and an amber light indicates its
reception. The inner marker signal frequency is 3,000
Hz, and a white light indicates its reception.

NOTE: The unit provides output for driving
external marker beacon lamps and it provides
a middle marker sense output for use with an
autopilot.

Marker Beacon Signal Augmentation
The HI SENS key can be pressed to augment marker
beacon signal reception sensitivity. The HI SENS function
is typically used either over airway markers or to receive
an earlier indication of a nearing outer marker during an
approach.
The middle marker sense indicator provides input to
the autopilot.

When the MKR/MUTE key is selected, the
corresponding annunciator light becomes illuminated
and the audio signal can be heard over the headsets.

The lamp and audio keying of the marker beacon receiver are summarized in Table 3-1.

When the MKR/MUTE key is annunciated and a
marker beacon tone is received, pressing the MKR/MUTE
key mutes the audio but does not affect the corresponding
annunciator light. The audio returns when the next (different) marker signal is received. If the MKR/MUTE key
is pressed while the marker beacon audio is muted, the
marker audio becomes deactivated and the MKR/MUTE
annunciator light is turned off.

Figure 3-4 Marker Beacon

NOTE: The marker beacon receiver lights operate
independently of the marker beacon audio and
cannot be turned off.

The marker beacon audio level is aligned at the factory
to produce its rated audio output. Audio output level is
also adjustable in Conﬁguration mode. Please consult a
Garmin-authorized service center for details.

NOTE: The marker beacon signal sensitivity
threshold can be set in Conﬁguration mode.
Please consult a Garmin-authorized service
center for details.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

Beacon
Outer Marker

Audio Frequency
400 Hz

Audio Keying
———

Middle Marker

1,300 Hz

•—•—

Airway/Inner Marker

3,000 Hz

••••

Rate
2 dashes per second
95 dot-dash combinations
per minute
6 dots per second

Lamp Color
Blue
Amber
White

Table 3-1 Marker Beacon Signal Characteristics

Inner Marker

Middle Marker
Figure 3-5 Marker Beacon Signal Indicator Lights on the PFD

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Outer Marker

SECTION 3 – AUDIO PANEL

3.4 RADIO INPUTS
Pressing DME, ADF, AUX, NAV1, or NAV2 selects
the corresponding audio source and activates the annunciator. Pressing the selected audio source key again deselects this audio source. Selected aircraft audio can be
heard over the appropriate headset and over the speakers
if SPKR is selected. Note that all aircraft radio keys can
be selected concurrently.

When no further aircraft radio activity is detected by
the unit, the amount of ambient background noise from
the radios is further reduced by the Master Avionics
Squelch (MASQTM) circuit.

If desired, the DME, ADF and AUX channels may be
disabled. Please consult a Garmin-authorized service center for details.

Figure 3-6 Aircraft Radios

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL

3.5 INTERCOM SYSTEM (ICS) ISOLATION
The intercom system (ICS) provides four (4) isolation
modes: ALL, PILOT, COPILOT, and CREW. The desired mode can be selected or deselected using the PILOT
and COPLT keys.

Figure 3-7 ICS Isolation

PILOT Mode

CREW Mode

PILOT mode is selected when only the PILOT key is
annunciated. In PILOT mode, the pilot can hear the selected radios, whereas the copilot and passengers can only
communicate with each other and hear MUSIC 1.

CREW mode is selected when both the PILOT and
COPLT keys are annunciated. In CREW mode, both the
pilot and copilot can hear the selected radios and MUSIC 1
and can also communicate with each other, while the passengers can only hear MUSIC 2.

COPILOT Mode
COPILOT mode is selected when only the COPLT key
is annunciated. In COPILOT mode, the copilot is isolated
from everyone and can only hear MUSIC 2. In this mode,
the pilot and passengers can hear the selected radios as
well as MUSIC 1 and can also communicate with each
other. The transitions between the possible ICS isolation
states are summarized in the table below.

Input
PILOT Key Press
COPLT Key Press

PILOT
ALL
CREW

ALL Mode
ALL mode is selected when neither the PILOT nor the
COPLT key is annunciated. In ALL mode, everyone hears
both the selected radios and MUSIC 1, and everyone is
able to communicate with everyone else.

Current ICS Isolation State
COPILOT
CREW
CREW
COPILOT
ALL
PILOT

ALL
PILOT
COPILOT

Table 3-2 ICS Isolation Mode Transitions

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL
The following table summarizes the ICS operation for
the four (4) ICS isolation modes supported by the unit.
ICS Isolation Mode
PILOT
(PILOT LED Lit)
COPILOT
(COPLT LED Lit)
CREW
(Both LEDs Lit)
ALL
(Both LEDs OFF)

Pilot Hears
Selected radios; pilot

Copilot Hears
Copilot; passengers; MUSIC 1

Passenger Hears
Copilot; passengers; MUSIC 1

Selected radios; pilot;
passengers; MUSIC 1
Selected radios; pilot; copilot;
MUSIC 1
Selected radios; pilot; copilot;
passengers; MUSIC 1

Copilot; MUSIC 2

Selected radios; pilot;
passengers; MUSIC 1
Passengers; MUSIC 2

Selected radios; pilot; copilot;
MUSIC 1
Selected radios; pilot; copilot;
passengers; MUSIC 1

Selected radios; pilot; copilot;
passengers; MUSIC 1

Table 3-3 ICS Operation Modes

3.6 VOLUME/SQUELCH CONTROL
When the GMA 1347 MAN SQ key is selected, pressing the VOL/SQ knob toggles between volume and
squelch adjustment modes. When the unit is in volume
adjustment mode, the VOL annunciation on the lower
left of the VOL/SQ knob is lit and volume can thus be
adjusted. Similarly, when the unit is in squelch mode, the
SQ annunciation on the lower right of the VOL/SQ knob
is lit and squelch threshold level can thus be adjusted.
NOTE: When the MAN SQ key is deselected (i.e.,
auto-squelch is active), pressing the VOL/SQ
knob has no effect on the VOL/SQ selection state
of the unit and VOL is automatically annunciated.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL
When transitioning from auto to manual squelch, the
unit “recalls” the previous VOL/SQ selection and sets the
state of the unit accordingly (see table below).
NOTE: The volume and squelch controls for the
COM and NAV radios are located on the PFD
and MFD bezels (please refer to the G1000 VHF
NAV/COM Pilot’s Guide for details).

Intercom VOL/SQ State
Intercom Volume Control
Intercom volume can be controlled via the VOL/SQ
knob. The small knob controls the pilot ICS volume,
while the large knob controls the copilot/passenger ICS
volume. Turning either knob clockwise increases audio
level. Conversely, turning either knob counterclockwise
decreases audio level. When the MAN SQ key is not annunciated, volume adjustment mode is automatically selected and the VOL annunciation is lit.
To adjust ICS volume when the MAN SQ key
is not annunciated:
1.

Turn the appropriate VOL/SQ knob.

To adjust ICS volume when the MAN SQ key
is annunciated, perform one of the following
steps:
1a. If the unit is in manual squelch threshold
adjustment mode (i.e., if the SQ annunciation
at the lower right of the VOL/SQ knob is lit),
press the VOL/SQ knob to toggle to ICS volume
adjustment mode, and turn the appropriate
VOL/SQ knob.

Intercom Squelch Threshold Control
Each microphone input has an automatic squelch
threshold. Manual squelch override as well as keyed ICS
operation (the latter to be used in noisier cockpit environments) is also available.
Manual squelch threshold adjustments can be performed via the VOL/SQ knob when the MAN SQ key is
annunciated and the SQ annunciation is lit. The small
VOL/SQ knob controls pilot squelch threshold adjustments, while the large VOL/SQ knob controls copilot/
passenger squelch threshold adjustments. Turning either
knob clockwise increases the squelch threshold level.
Conversely, turning either knob counterclockwise decreases the squelch threshold level.
NOTE: In manual squelch mode, all crew audio
inputs can break squelch when the VOL/SQ knob
is adjusted to minimum. When the VOL/SQ knob
is adjusted to maximum, the ICS only produces
audio when the ICS PTT is pressed.

To adjust squelch threshold level manually
if the MAN SQ key is not annunciated:
1.

Press the MAN SQ key and perform one of the
following steps:

2a. If the VOL annunciation is lit, press the VOL/SQ
knob to illuminate the SQ annunciation, and
turn the VOL/SQ knob.
2b. If the SQ annunciation is already lit, turn the
VOL/SQ knob.

1b. If the unit is already in ICS volume adjustment
mode (i.e., if the VOL annunciation at the
lower left of the VOL/SQ knob is lit), turn the
appropriate VOL/SQ knob.
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 3 – AUDIO PANEL
To adjust squelch threshold level manually
if the MAN SQ key is already annunciated:
1a. If the VOL annunciation is lit, press the VOL/SQ
knob to illuminate the SQ annunciation, and
turn the VOL/SQ knob.
1b. If the SQ annunciation is already lit, turn the
VOL/SQ knob.

3.7 DISPLAY BACKUP MODE
Pressing the red DISPLAY BACKUP button located
at the bottom of the audio panel selects the reversionary
(or backup) mode for all displays. Reversionary mode
is a mode of operation in which both the PFD and MFD
are identically conﬁgured to display all of the important
ﬂight parameters in the event of display failure. See the
Introduction Section of this Cockpit Reference guide for
complete details.

Figure 3-8 Reversionary Mode

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

SECTION 4: MULTI FUNCTION
DISPLAY
4.1 INTRODUCTION
This section of the G1000 Cockpit Reference Guide
introduces the pilot to the major features of the Multi
Function Display. A complete description of the MFD
with detailed operating procedures is contained in the
G1000 Multi Function Pilot’s Guide and the G1000
Engine Indication System Pilot’s Guide.

LTNG – Press to display lightning data on the
Navigation Map Page (within a 200 nm
radius of the aircraft).
BACK – pressing the BACK softkey displays
the ENGINE and MAP top level softkeys.
DCLTR (declutter) – pressing the DCLTR softkey
removes map information in three levels..

4.2 MFD SOFTKEYS
The MFD softkeys are located below the display
glass and provide control over ﬂight management functions which includes GPS and NAV management, engine
and airframe monitoring, terrain, weather, and trafﬁc.
Figure 4-1 shows an MFD ﬂowchart identifying what
functions are available via the softkey labels.
The MFD softkeys perform the following functions:
ENGINE – Pressing the ENGINE softkey makes
available the LEAN and SYSTEM softkeys which
in turn access the Lean Page and the System Page,
respectively.
MAP – pressing the MAP softkey enables the following softkeys:
TRAFFIC – pressing the TRAFFIC softkey
displays/removes Trafﬁc on the Navigation
Map.
TOPO – pressing the TOPO softkey displays
or removes topographic information on the
Navigation Map.
TERRAIN – pressing the TERRAIN softkey
displays/removes terrain and obstacle data
on the Navigation Map.
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

ENGINE

MAP

DCLTR

CHKLIST

NOTE: Nav III does not use the checklist
functionality which exists in the G1000

Press the BACK softkey on this level to
return to the top softkey level

ENGINE

LEAN

SYSTEM

DCLTR-1

BACK

DCLTR-2

DCLTR-3
Press the BACK softkey on this level to
return to the top softkey level

ENGINE

LEAN

SYSTEM

CYL SLCT

ASSIST

Press the BACK softkey on this level to
return to the top softkey level

BACK

TRAFFIC

Press the BACK softkey on this level to
return to the top softkey level

Press the ENGINE softkey on any level to
return to the LEAN and SYSTEM softkey level

ENGINE

LEAN

TOPO

SYSTEM

RST USED

BACK

Figure 4-2 MFD Softkeys

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

TERRAIN

LTNG

BACK

SECTION 4 – MFD

4.3 ENGINE INDICATION SYSTEM
WINDOW
The G1000 Engine Indication System (EIS) window
provides gauges, bar graphs and numeric readouts of engine and airframe systems parameters to the pilot. The
EIS window is displayed on the left side of the MFD during normal operations. In reversionary mode, the PFD
and MFD both show the EIS window.
The EIS contains three distinct pages, which are
accessed by the ENGINE softkey:

Manifold Pressure Gauge
The Manifold Pressure gauge displays the engine power
in inches of mercury (in Hg). There are two color bands on
the Manifold Pressure gauge, green and red.
• Green – Normal operating range.
• Red – (Top of arc) – Maximum manifold pressure.

Tachometer
The Tachometer displays propeller speed in revolutions per minute (RPM). There are three color bands on
the Tachometer.
• White – Below normal ﬂight operating range.
• Green – Normal ﬂight operating range.
• Red – Indicates propeller overspeed.

• Engine (default)
• Lean
• System

Fuel Qty Indicator

ENGINE Page
The Engine page is the default EIS page, which displays
engine, fuel and airframe/electrical indicators. Atop this
page are round dial gauges with a white pointer and digital
readouts for manifold pressure and revolutions per minute
(RPM). Below those gauges are color-coded horizontal bar
indicators with triangle pointers and numeric readouts indicating fuel quantity (no numeric readout), fuel ﬂow (not
color-coded), oil pressure, oil temperature, exhaust gas
temperature (EGT) of the hottest cylinder – for normally
aspirated aircraft, turbine inlet temperature (TIT) – for turbocharged aircraft, and cylinder head temperature (CHT)
of the hottest cylinder. The pointer on the horizontal bar
indicators appears in white, which represents acceptable
areas of operation. The pointer color changes to yellow or
red upon exceeding areas of normal operation.
The green band is indicative of normal areas of operation. Located at the bottom of the page are the electrical
indicators. A numeric readout is provided for the battery
voltage, essential bus voltage, and the alternator amperage.

The Fuel Quantity indicator displays the quantity of
fuel in the tanks in gallons. The indicator ranges from E
(Empty) to F (Full) with tick marks at 10, 20, 30, and 40
gallons. Two triangle pointers labeled L (Left) and R (Right)
indicate the number of gallons in each fuel tank. There are
two color bands on the Fuel Quantity indicator.
• Yellow – Caution
• Red – Warning
NOTE: The Fuel Quantity Indicator will only display to 50 gallons when full, regardless of actual
maximum capacity.
NOTE: The pilot should refer to the Aircraft Flight
Manual Supplement (AFMS) for actual minimum/
maximum operating parameters associated with
EIS display indications.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Manifold
Pressure
Gauge

Tachometer

Fuel Quantity
Indicator

Fuel Flow
Indicator
Oil Pressure
Indicator
Oil Temperature
Indicator
Exhaust Gas
Temperature
Cylinder Head
Temperature
Indicator
Voltmeter
Ammeter

Flaps Position
Indicator

Turbine Inlet
Temperature
Indicator

Elevator Trim
Indicator

Rudder Trim
Indicator
Figure 4-3 ENGINE Page (Normally Aspirated)

Figure 4-4 ENGINE Page (Turbocharged)

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Fuel Flow Indicator (Normally Aspirated)

CHT Indicator

The Fuel Flow indicator displays current fuel ﬂow values, expressed in gallons per hour (GPH).

The CHT (Cylinder Head Temperature) indicator displays the temperature of the hottest cylinder in degrees
Fahrenheit. The number of the hottest cylinder appears
in the triangle pointer.
• Green – Normal
• Red – Warning

Fuel Pressure Indicator (Turbocharged Only)
The Fuel Pressure indicator displays current fuel system pressure in pounds per square inch (PSI).
• Green – Normal
• Yellow – Caution (low and high)
• Red – Warning (minimum and maximum)

Oil Pressure Indicator
The Oil Pressure indicator displays the pressure of
the oil supplied to the engine in pounds per square inch
(PSI).
• Green – Normal
• Yellow – Caution (low and high)
• Red – Warning (minimum and maximum)

Oil Temperature Indicator
The Oil Temperature indicator displays the engine oil
temperature in degrees Fahrenheit.
• Green – Normal
• Red – Warning

EGT Indicator (Normally Aspirated)
The EGT (Exhaust Gas Temperature) indicator displays
the exhaust gas temperature of the hottest cylinder in degrees Fahrenheit. The number of the associated cylinder
is indicated in the triangle pointer. The EGT indicator
does not have color bands.

TIT Indicator (Turbocharged Only)
The TIT (Turbine Inlet Temperature) indicator displays
the temperature at the turbine inlet in degrees Fahrenheit.
• Green – Normal
• Red – Warning

Voltmeter
The Voltmeter displays the battery and essential bus
voltage.

Ammeter
The Ammeter displays the alternator load in amperes.

Rudder Trim Indicator
The Rudder Trim indicator depicts the position (right/
left) of the rudder trim setting. Actual trim position is
shown using a blue inverted triangle. The ‘takeoff’ rudder
trim position is shown in white.

Elevator Trim Indicator
The Elevator Trim indicator depicts the position (up/
down) of the elevelator trim setting. Trim position is
shown by a blue triangle. A white block indicates ‘takeoff’
elevator trim position.

Flaps Position Indicator
The Flaps Position Indicator shows the current position of the ﬂaps. The three possible positions, up, takeoff, and down, are depicted in cyan as ‘UP’, ‘T/O’, and
‘DN’, respectively. During ﬂaps position transition, ‘///’ is
displayed in the window.
NOTE: The Lean and System pages are
described in detail in the G1000 Engine
Indication System Pilot’s Guide.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

4.3 MFD PAGE GROUPS
The MFD displays GPS/Navigation ﬂight information
in the following page groups:
• Map (MAP):
Navigation Map Page
Trafﬁc Map Page
Weather Map Page
Terrain Proximity Page
• Waypoint (WPT) :
Airport Information Page
Intersection Information Page
NDB Information Page
VOR Information Page
User Waypoint Information Page
• Auxiliary (AUX):
Trip Planning Page
Utility Page
GPS Status Page
System Setup Page
System Status Page
• Nearest (NRST):
Nearest Airports Page
Nearest Intersections Page
Nearest NDB Page
Nearest VOR Page
Nearest User Waypoints Page
Nearest Frequencies Page
Neatest Airspaces Page

To select a speciﬁc page group:
1.

Turn the large FMS knob until the desired page
group is selected.
Active Page group is
highlighted

Currently
selected page is
highlighted

Figure 4-5 Page Group Window

To select a different page within the group:
1.

Turn the small FMS knob. As the knob is turned,
the bottom right corner of each page indicates
the page group that is currently being displayed
(e.g., MAP or NRST, etc.), the number of
screens available within that group (indicated
by rectangle icons) and the placement of the
current page within that group (indicated by a
solid cyan rectangle icon). The page group and
active page title window are displayed above
the nav map display.
Page Group

Active Page Title

Figure 4-6 Page Title Window

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Working With Menus
Much of the operation of the G1000 is accomplished
using a menu interface. The G1000 has a bezel-mounted
dedicated menu key that when pressed, displays a context-sensitive list of options. This options list allows the
pilot to access additional features or make settings changes
which speciﬁcally relate to the currently displayed page.
Some menus provide access to additional submenus that
are used to view, edit, select, and, review options. Some
menus display ‘NO OPTIONS’ when there are no options
for the page selected.

There may be more options than can be displayed so
you may have to turn the small or large FMS knob to
scroll through the list to identify them. In all cases, once
the menu is displayed the small or large FMS knob is
turned to highlight an item and the ENT key is pressed
to select that item or the CLR key removes the menu and
cancels the operation. Pressing the softkeys does not
display a menu or submenu.

The main keys which are used in association with all
page group operations are listed below:
• CLR – erases information or cancels an entry.
Press and hold CLR to immediately display the
Navigation Map Page, regardless of the page currently displayed.
• ENT – accepts a menu selection or data entry.
Approves an operation or completes data entry.
Also, conﬁrms information.
• BACK – resets the MFD softkeys to their default
settings (ENGINE, MAP, DCLTR, MODE, VIEW,
etc).
• DCLTR – removes information from the moving
map in a progressive manner with each key-press.
• MENU – displays a context-sensitive list of
options that allows access to additional features or
that allows the pilot to change the settings which
relate to the currently displayed page.

Figure 4-6 Menu With Options

Figure 4-7 Menu With No Options

NOTE: Data is entered using the large and small
FMS knob. Practice with them to become efﬁcient at entering data. This will greatly reduce
the amount time spent operating the MFD in
ﬂight.
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

4.4 NAVIGATION MAP PAGE
The Navigation Map Page provides an extensive array of GPS/navigation/mapping capability.
Key features include:
• Map display showing airports, navaids, airspaces,
land data (highways, cities, lakes, rivers, borders,
etc.) with names (labels)
• Map pointer information (distance and bearing
to pointer, location of pointer, name and other
pertinent information)
• TIS Trafﬁc Display
• Lightning Display (optional with WX-500 installation)
• Obstacle Display
• Map Zoom Range Legend
• Wind Direction and Speed
• Heading Indication
• Aircraft icon representing present position
• Icons for enabled map features
• Track Vector
• Topography Scale
• Fuel Range Ring
• Topography Data
• Terrain Proximity Data
Appendix F lists all of the display features provided by
the Navigation Map Page.
WARNING: The Navigation Map page display
should be used only for non-navigational situational awareness and not for navigation. Any
map display indication should be compared with
approved navigation sources.

To select the Navigation Map Page:
1.

Turn the large FMS knob to select the Map Page
group.

Turn the small FMS knob to select the
Navigation Map Page. The page group name
and page title is displayed below the navigation status bar; ‘MAP – NAVIGATION MAP’.
NOTE: In addition to turning the large and small
FMS knobs, the Navigation Map Page can be
selected from any page by pressing and holding
the CLR (DFLT MAP) key.

Navigation Map Page Operations
The following Navigation Map Page operations can be
performed:
•
•
•
•
•
•
•
•
•
•
•
•
•
•

Changing the Map Orientation
Clearing Lightning Data
Selecting a Map Range
Using the Auto Zoom Feature
Identifying Aviation Map Data
Decluttering the Map
Panning the Map
Displaying Topographic Information on the
Navigation Map Page
Displaying Terrain Information on the Navigation
Map Page
Displaying Trafﬁc on the Navigation Map Page
Displaying Lighting Data on the Navigation Map
Page
Displaying Obstacles
MFD Navigation Status Window
Navigation Map Page Options Menu

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Figure 4-8 Navigation Map Page

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Changing the Map Orientation
See the Navigation Map Page Menu section for instructions on how to change the map orientation.
Clearing Lightning Data
See the Navigation Map Page Menu section for instructions on how to clear lightning data from the map display
NOTE: A complete list of available map datums
are given in Appendix D of the Pilot’s Guide.

Selecting a Map Range

Using the Auto Zoom Feature
The auto zoom feature automatically adjusts the map
from an enroute range of 2000 nm through each lower range,
stopping at a range of 1.5 nm as the aircraft approaches the
destination waypoint. See the Navigation Map Page Menu
section for instructions on enabling/disabling the auto zoom
feature.
Identifying Aviation Map Data
See Appendix F of the Pilot’s Guide Appendices as well
as the MFD Pilot’s Guide for a complete description of
the map symbology used on the Navigation Map Page.

The Navigation Map Page can be set to 28 different
range settings from 500 feet to 2000 nautical miles. The
current range is indicated in the lower right corner of the
Navigation Map Page and represents the top-to-bottom
distance covered by the map. To change the map range
turn the joystick counter-clockwise to zoom in, turn it
clockwise to zoom out.

Map
Range

Figure 4-9 Navigation Map Range

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Decluttering the Map

To pan the map:

The Navigation Map Page can be quickly decluttered
by repeatedly pressing the DCLTR softkey until the desired
detail is depicted. The declutter level label appears above
the DCLTR softkey. Table 8.2.1 lists the map features that
are turned off at each declutter level.

Push in the joystick to display the panning
arrow.

Push in and move the joystick in the general
direction of the desired destination to place
the panning arrow at the destination location. When the panning arrow is placed on an
object, the name of the object is highlighted
(even if the name wasn’t originally displayed
on the map). This feature applies to everything
displayed on the map except route lines. When
any map feature or object is selected on the
map display, features or objects are displayed
in the box located at the top of the display.
From here, the pilot can designate the waypoint as the Direct-to destination. When the
panning arrow crosses an airspace boundary,
the boundary is highlighted and airspace information is displayed at the top of the display.

To remove the panning arrow and return to
the present position, push in the joystick.

NOTE: Some of the map features are automatically removed at certain zoom ranges due to the
map setup conﬁguration for each map item.
NOTE: “SUA” listed in the table below stands
for Special Use Airspace. These are controlled
airspaces, military zones, etc.

Map Panning
Map panning moves the map beyond its current limits
without adjusting the map range. When the panning function is selected by pushing in the joystick, a panning arrow ﬂashes on the map display. A window also appears at
the top of the map display showing the latitude/longitude
position of the pointer, the bearing and distance to the
pointer from the aircraft’s present position, and the elevation of the land at the position of the pointer. When the
panning arrow crosses an airspace boundary, the boundary is highlighted and airspace information is displayed at
the top of the display. The information includes the name
and class of airspace, the ceiling in feet expressed in Mean
Seal Level (MSL), and the ﬂoor in feet MSL.
NOTE: The airspace boundary stays highlighted
for approximately four seconds before returning
to normal shading.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Latitude and
longitude
position of
pointer

Distance, bearing
and elevation

Panning
Arrow

Figure 4-10 Navigation Map Panning

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Displaying Topographic Data on the Navigation
Map Page
The Navigation Map Page displays various shades of
topography land colors representing the rise and fall of
land elevation similar to aviation sectional charts. The
Navigation Map Page can display a topographic scale
representing various key points of terrain elevation colors
with their associated elevation value labeled.
To display topographic data on the Navigation Map Page:
1.

Press the MAP softkey.

Press the TOPO softkey. Topo data can also
be displayed on the Navigation Map Page by
using the ‘On/Off’ topo data map setup feature.
See the Navigation Map Page setup menu section.

Displaying Terrain Data on the Navigation Map
Page
Terrain data can be displayed on the Navigation Map Page by pressing the TERRAIN softkey. Terrain symbology (mountain icons) appear next to the
map range in the bottom right corner of the page indicating the presence of terrain data on the map. See
the Terrain Proximity Page section for a terrain color
interpretation chart.
To display terrain data on the Navigation
Map Page:
1.

Press the MAP softkey.

Press the TERRAIN softkey. Press the TERRAIN
softkey again to remove terrain data from the
Navigation Map Page.

TRAFFIC softkey

TOPO softkey
TERRAIN softkey

Figure 4-11 TRAFFIC, TOPO and TERRAIN Softkeys

Displaying Trafﬁc on the Navigation Map Page
Pressing the TRAFFIC softkey displays Trafﬁc Information Service (TIS) trafﬁc on the Navigation Map Page. TIS
is a ground-based service providing relative location of all
ATCRBS Mode-A and Mode-C transponder equipped aircraft within a speciﬁed service volume. The TIS ground
sensor uses real time track reports to generate trafﬁc
notiﬁcation. Surveillance data includes all transponderequipped aircraft within the coverage volume. The G1000
displays up to eight trafﬁc targets within a 7.5 nautical
mile radius, from 3,000 feet below to 3,500 feet above the
requesting aircraft. See Appendix E of the Pilot’s Guide
Appendices for a full description of TIS. A trafﬁc symbol
appears next to the map range in the bottom right corner
of the display indicating the presence of trafﬁc data on
the map.
To display trafﬁc on the Navigation Map
Page:
1.

Press the MAP softkey.

Press the TRAFFIC softkey. Press the
TRAFFIC softkey again to remove trafﬁc from the
Navigation Map Page.
NOTE: Traffic and terrain data can also be
displayed by using the ‘On/Off’ Navigation Map
Page option. See the Navigation Map Page setup
section for details.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
To display trafﬁc on the Navigation Map
Page:
1.

Press the MAP softkey.

Press the TRAFFIC softkey. Press the
TRAFFIC softkey again to remove trafﬁc.
NOTE: Traffic and terrain data can also be
displayed by using the ‘On/Off’ Navigation Map
Page option. See the Navigation Map Page setup
section for details.

Displaying Lightning Data on the Navigation Map
Page
Pressing the LTNG softkey after pressing the MAP
softkey displays WX-500 Stormscope data on the Navigation Map Page within a maximum of 200 nm radius of the
aircraft. The Navigation Map Page displays cell or strike
information using yellow lightning strike symbology.
This added capability improves situational awareness,
which makes it much easier for the pilot to relate storm
activity to airports, navaids, obstacles and other ground
references.
To display lightning data on the Navigation
Map Page:
1.

Press the MAP softkey.

Press the LTNG softkey. Press the LTNG
softkey again to remove lightning data from
the Navigation Map Page
Onscreen map maximum
elevation
Onscreen map minimum
elevation

Aircraft altitude
Ground elevation

Figure 4-12 Topography Scale

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
In normal operation, the current mode and rate
are displayed in the top right corner of the Navigation
Map Page. The mode is described by the word ‘STRIKE’
when in strike mode, or ‘CELL’ when in cell mode.

• Vertical speed required (VSR)
• Cross track error (XTK)
• Currently selected MFD page title

The strike data display phases are:
1. Lightning Symbol (latest strikes; less than one
minute; a black guard band is placed around
the strike symbol during the ﬁrst six seconds of
display)
2. Large Plus ‘+’ sign (more than one minute old)

Figure 4-13 MFD Navigation Status Window

NOTE: Instructions on changing a data ﬁeld on
the MFD Navigation Status Window is given in
the System Setup Section.

3. Small Plus ‘+’ sign (more than two minutes old)
4. Strike Data is no longer displayed (after three
minutes)
Lightning Data Display Range

Lightning data can be displayed up to 800 nm zoom
range, but the data only goes out as far as the Stormscope can report (200 nm). The 500 nm zoom range
will display all lightning data. Ranges greater than 500
nm do not display any further Stormscope data.

MFD Navigation Status Window
The MFD Navigation Status Window displays four,
user-conﬁgurable ﬁelds which can show the following
data:
•
•
•
•
•
•
•
•
•
•

Bearing to next waypoint (BRG)
Distance to next waypoint (DIS)
Desired track to next waypoint (DTK)
En-route safe altitude (ESA)
Estimated Time of Arrival (ETA)
Estimated Time Enroute (ETE)
Ground Speed (GS)
Maximum Safe Altitude (MSA)
Track angle error (TKE)
Track angle (TRK)
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Navigation Map Page Menu
The Navigation Map Page can be customized using
three page menu options: ‘Map Setup’, ‘Measure
Bearing/Distance’, and ‘Clear Lightning Data’. To display
the page menu, press the MENU key (with the Navigation
Map Page displayed).

Figure 4-14 Navigation Map Page Menu Options

First Option: ‘MAP SETUP’
The ﬁrst option is ‘MAP SETUP’. There are ﬁve
“groups” available under the ‘MAP SETUP’ option: Map,
Weather, Trafﬁc, Aviation, and Land. The Map Group is
discussed in detail in the MFD Pilot’s Guide.

• Heading Up (HDG up) ﬁxes the top of the map
display to the current aircraft heading.
To change the map orientation:
1.

With the Navigation Map Page displayed,
press the MENU key to display the Navigation
Map Page Menu. The cursor ﬂashes on ‘Map
Setup’.

Press the ENT key. The Map Setup Menu is
displayed.

Turn the small FMS knob to select the ‘Map’
group and press the ENT key.

Turn the large FMS knob to highlight the
‘ORIENTATION’ ﬁeld.

Turn the small FMS knob to select the desired
orientation and press the ENT key.

Press the FMS knob to return to the Navigation
Map Page.

Map Group
There are eleven options in the Map Group. The ﬁrst
is ‘ORIENTATION’.
Orientation
There are four map orientation selections: ‘North up’,
‘Track up’, ‘DTK up’, and ‘HDG up’.
• North up ﬁxes the top of the map to a north heading (default map setting).
• Track up adjusts the top of the map display to the
current track heading.
• Desired Track Up (DTK up) ﬁxes the top of the
map display to the desired course.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

4.5 TRAFFIC MAP PAGE
The Trafﬁc Map Page displays the following information:
• Current aircraft location, surrounding Trafﬁc
Information System (TIS) trafﬁc, and range marking rings.
• The current trafﬁc mode (OPERATE, STANDBY).
• A trafﬁc alert message (FAILED, DATA FAILED,
NO DATA, UNAVAILABLE).
• Trafﬁc display banner (AGE 00:, TRFC COAST,
TA OFF SCALE, TRFC RMVD, TRFC FAIL, NO
TRFC DATA, TRFC UNAVAIL, TRAFFIC).
To select the Trafﬁc Map Page:
1.

Select the MAP group of pages. Turn the small
FMS knob to select the Trafﬁc Map Page.

CAUTION: TIS warns the pilot with voice and
visual trafﬁc advisories whenever it predicts an
intruder to be a threat. The pilot should not start
evasive maneuvers using information from the
Trafﬁc Map Page display or on a trafﬁc advisory
only. The display and advisories are intended
only for assistance in visually locating the trafﬁc
and lack the resolution and coordination ability
necessary for evasive maneuvering. The pilot
should attempt to visually acquire the intruder
aircraft and maintain/attain a safe separation
in accordance with the regulatory requirements
and good operating practice. If the pilot cannot
acquire the aircraft, they should contact ATC to
obtain any information that may assist concerning the intruder aircraft. Based on the above
procedures minor adjustment to the vertical
ﬂight path consistent with air trafﬁc requirements are not considered evasive maneuvers.
See Appendix E in the Pilot’s guide for detailed
TIS information.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Trafﬁc Mode

Map Range
Trafﬁc

Vehicle (ownship)

Figure 4-15 Trafﬁc Map Page

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SECTION 4 – MFD

TIS Symbology

Trafﬁc Map Page Operations

TIS trafﬁc is displayed on the Trafﬁc Map Page according to TCAS symbology. A Trafﬁc Advisory (TA) symbol
is displayed as a solid yellow circle (or half circle on the
outer range ring if the trafﬁc is outside the range of the
dedicated trafﬁc page). All other trafﬁc is displayed as a
hollow white diamond. Altitude deviation from the user’s
aircraft altitude is displayed above the target symbol if
they are above own aircraft altitude, and below the symbol if they are below own aircraft altitude. Altitude trend
is displayed as an up arrow (+500 ft/min), down arrow
(-500 ft/min), or no symbol if less than 500 ft/min rate in
either direction. Other symbols:
• Other Trafﬁc – this symbol represents trafﬁc
detected within the selected display range that
does not generate a TA.
• Trafﬁc Advisory (TA) – this symbol is generated
when trafﬁc meets the advisory criteria described
previously.
• Trafﬁc Ground Track is indicated on the Trafﬁc
Map Page by a “target track vector”. The track
vector line is projected from the trafﬁc advisory
symbol and is drawn at any angle necessary to
represent the current track of the trafﬁc advisory
data.
Item

Power-Up Test
The TIS interface performs an automatic test during
power-up. If the system passes the power-up test, the
standby screen is displayed on the Trafﬁc Map Page. If the
system passes the power-up test, and the aircraft is airborne, trafﬁc is displayed on the Trafﬁc Page in the operating mode.
If the system fails the power up test, the ‘NO DATA’,
‘DATA FAILED’, or ‘FAILED’ message is displayed. Contact your Mooney service center or Garmin dealer for corrective action if the ‘DATA FAILED’, or ‘FAILED’ message
is displayed. The ‘FAILED’ message indicates the GTX
33 transponder has failed. The ‘DATA FAILED’ message
indicates data is being received from the GTX 33 but a
failure was detected in the data stream. The ‘NO DATA’
message indicates that data is not being received from the
GTX 33.
Changing the Map Range
To change the map range:
1.

Turn the joystick clockwise to zoom out, or turn
the joystick counter-clockwise to zoom in. Map
ranges are 2 nm, 6 nm, and 12 nm.

Symbol
NOTE: Trafﬁc Information Service (TIS) is not
available in all areas.

Trafﬁc
Proximate Trafﬁc
Trafﬁc Advisory, Out of Range
Trafﬁc Advisory

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SECTION 4 – MFD
Operating Mode

Once the aircraft is airborne (determined by system conﬁguration at the time of installation) the system
switches from standby mode to operating mode. The
G1000 displays ‘OPERATE’ in the upper left hand corner
of the display and begins to display trafﬁc on the Trafﬁc or
Map Page. The TIS Trafﬁc Advisory (TA) should alert
the crew to use additional vigilance to identify the intruding aircraft. Any time the trafﬁc symbol becomes a
yellow circle or a voice warning is announced, conduct
a visual search for the intruder. Maintain visual contact to ensure safe operation.
Once the aircraft is on the ground (determined by
system conﬁguration at the time of installation) the
system switches from operating mode to standby mode. The
Trafﬁc Map Page displays ‘STANDBY’.
• STANDBY – when the Trafﬁc Map Page displays
‘STANDBY’ in the status box located in the upper
left corner of the Trafﬁc Map Page, the TIS system
is in standby mode and cannot display trafﬁc data.
• OPERATE – when the Trafﬁc Map Page displays
‘OPERATE’ in the status box located in the left
corner of the Trafﬁc Map Page, the TIS system is
in operational mode and available to display trafﬁc on the Trafﬁc or Map Page.

Press the MENU key. The page menu is
displayed with ‘Standby Mode’ or ‘Operate
Mode’ highlighted. Press the ENT key on the
desired selection.

TIS Audio Alert
A TIS audio alert is generated whenever the number
of TAs on the Trafﬁc Map Page display increases from one
scan to the next. The limiting to TAs only reduces the
amount of “nuisance” alerting due to proximate aircraft.
For example, when the ﬁrst TA is displayed, the pilot is
alerted audibly. So long as a single TA aircraft remains on
the TIS display, no further audio alert is generated. If a
second (or more) TA aircraft appear on the display, a new
audio alert is sounded. If the number of TAs on the TIS
display decreases and then increases, a new audio alert is
sounded. The TIS audio alert is also generated whenever
TIS service becomes unavailable. The volume of the audio alert (including the choice between a male or female
voice) is conﬁgured during installation. The following
TIS audio alerts are available:
• “Trafﬁc” - TIS trafﬁc alert is received.
• “Trafﬁc Not Available” - TIS service is not available
or out of range.

The pilot can switch between the standby (STBY) and
operate (ON) modes of operation to manually override
automatic operation using the page menu or softkeys.
To switch between operating modes:

Press the MODE softkey.

Press the STBY or ON softkey to switch between
modes. ‘STANDBY’ or ‘OPERATE’ is displayed
in the status box located in the upper left
corner of the Trafﬁc Map Page OR:
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SECTION 4 – MFD
TIS Trafﬁc Status
The MFD indicates the following TIS trafﬁc status to
the pilot.
Trafﬁc Banner
• AGE - if trafﬁc data is not refreshed within 6
seconds, an age indicator (i.e., ‘AGE 00:06’) is
displayed in the lower left corner of the display (when displaying trafﬁc). After another 6
seconds, if data is still not received, the trafﬁc
is removed from the display. The pilot should
be aware that the quality of displayed trafﬁc is
reduced in this condition.
• TRFC COAST - the ‘TRFC COAST’ (trafﬁc coasting) banner located above the AGE timer indicates
that displayed trafﬁc is held even though the data
is stale. The pilot should be aware that the quality
of displayed trafﬁc is reduced in this condition.
• TRFC RMVD - the ‘TRFC RMVD’ banner indicates
that trafﬁc has been removed from the display due
to the age of the data being too old to “coast” (for
the time period of 12-60 seconds from the last
receipt of a TIS message). The pilot should be
aware that trafﬁc may be present but not shown.

• TA OFF - the ‘TA OFF’ scale banner displayed in
the lower left corner of the display indicates that
a trafﬁc advisory is outside the selected display
range. The trafﬁc advisory off range banner is
removed when the trafﬁc advisory is within the
selected display range.
• TRAFFIC - on the PFD, when the system receives
a trafﬁc advisory a ﬂashing ‘TRAFFIC’ alert is
displayed in the upper left hand portion of the
display. The PFD inset map also automatically
displays trafﬁc data.

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SECTION 4 – MFD

4.6 WEATHER MAP PAGE
The G1000 provides an optional display interface for the
L-3 Stormscope® WX-500 Series II Weather Mapping
Sensor. The WX-500 is a passive weather avoidance
system that detects electrical discharges associated with
thunderstorms within a 200 nm radius of the aircraft.
The Stormscope measures relative bearing and distance
of thunderstorm related electrical activity and displays the
information on the Weather Map Page.
NOTE: Refer to the WX-500 User’s Guide for a
detailed description of the Stormscope.

The Weather Map Page displays the following
information:
• Map showing surrounding lightning strikes (in
strike or cell mode), current aircraft location, and
range marking rings, in 360° mode or 120° mode.
• Current lightning mode.
• Current strike rate.
• Wind vector.
• Heading direction.
• Current weather data status, or none if no
problems with weather data are detected
• Map orientation.
• North arrow indicator, when in “track-up” mode.
• Active Flight Plan or Direct-to Navigation.

Display Mode

Current Strike Rate

Range
Marking Rings

Figure 4-16 Weather Map Page

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SECTION 4 – MFD

NOTE: The WX-500 has to be receiving valid
heading information in order for lightning data
to be displayed.

To change the viewing mode between 360˚
and 120˚:
1.

Select the Weather Map Page.

Press the VIEW softkey. The 360 and ARC softkeys are displayed. Press the 360 softkey to
display a 360˚ viewing are or press the ARC
softkey to display a 120˚ viewing area OR:

Press the MENU key. The page menu is
displayed with ‘View Arc’ or ‘View 360’ highlighted. Press the ENT key on the desired
selection.

Weather Display Information
For weather display interpretation, the examples in the
WX-500 User’s Guide are designed to help the pilot relate
the cell or strike patterns shown on the Weather Map Page
to the size and location of thunderstorms that may be near
the aircraft.

Weather Map Page Operations
The following Weather Map Page operations can be
performed using softkeys or page menu options:
• Changing lightning mode between cell and strike
• Changing viewing mode between 360° and 120°
ARC.
• Clearing lightning data.
To change lightning mode between cell and
strike:
1.

Select the Weather Map Page.

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 Weather Map
Page OR:

Press the MENU key. The page menu is
displayed with ‘Strike Mode’ or ‘Cell Mode’
highlighted. Press the ENT key on the desired
selection.

To clear display lightning data from the
display:
Press the CLEAR softkey to remove all lightning
data from the display OR: Press the MENU key.
Select ‘Clear Lightning Data’. Press the ENT
key.
To change the display range, turn the joystick
clockwise to zoom out or turn the joystick counter-clockwise to zoom in. Display ranges are 25 nm, (25 and 50)
nm, (50 and 100) nm, and (100 and 200) nm
1.

NOTE: An active flight plan or Direct-to is
displayed on the Weather Map Page if one is
available and is within the display range.

Lightning Strike Symbols
Item
Lightning Strike - Age is 0 - 6 Seconds

Symbol

Lightning Strike - Age is 6 - 20 Seconds
Lightning Strike - Age is 20 - 60 Seconds
Lightning Strike - Age is 60 - 120 Seconds

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SECTION 4 – MFD

4.7 TERRAIN PROXIMITY PAGE

Terrain Proximity Page Operations

CAUTION: Terrain and obstacle data are provided
only as an aid to situational awareness. No aural
messages or textual annunciations are displayed
to the pilot during ﬂight operations regarding the
presence of terrain or obstacles.

The Terrain Proximity Page displays the following:
• Current aircraft location.
• Range marking rings (25 nm, 25/50 nm, 50/100
nm, and 100/200 nm).
• Heading Box (North Up, Track Up, DTK Up,
HDG Up). Heading on the Terrain Proximity Page
displays ‘HDG Up’ map data unless there is no
valid heading.

There are two terrain/obstacle viewing options available (relative to the position of the aircraft), a radar-like
ARC (120°) display and a 360° default display.
To change the viewing mode between 360°
and ARC:
1.

Select the Terrain Proximity Page

Press the VIEW softkey. Press the ARC softkey.

To return to the 360 degree viewing display
press the 360 softkey OR:

Press the MENU key. The page menu is
displayed with ‘View Arc’ or ‘View 360º’
highlighted. Press the ENT key on the desired
selection.

To change the map range on the Terrain
Proximity Page:
1.

Turn the joystick clockwise zoom out or turn
the joystick counter-clockwise zoom in. Map
ranges are 25 nm, 25/50 nm, 50/100 nm, and
100/200 nm.

Aircraft Altitude
100' Threshold

1000' AGL

Figure 4-17 Terrain Scale

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SECTION 4 – MFD

Displaying Obstacle Data

Navigation Map Display Conditions

The Terrain Proximity Page displays obstacle data
with heights greater than 200 feet Above Ground Level
(AGL) located at their geographical position location
throughout the world. Obstacles are displayed in
three levels:
• SAFE
• CAUTION
• WARNING
Each level is associated with a color. The G1000
will adjust colors on the Terrain Proximity Page automatically as the aircraft altitude changes.
Obstacle
Color
RED
YELLOW
GRAY

Indication
WARNING: Obstacle height is at or above
100’ below the current aircraft altitude.
CAUTION: Obstacle height is between
100’ and 1000’ below the current aircraft
altitude.
SAFE: Obstacle height is lower than
1000’ below the current aircraft altitude.

The Map Setup Page Menu has ‘OBSTACLE’ and
‘TERRAIN feature On/Off options. The Terrain Proximity
Page displays or does not display obstacles on the Navigation Map Page based on the selection of each as summarized in the table below:
TERRAIN OBSTACLE
FEATURE FEATURE

TERRAIN PROXIMITY PAGE

OFF

NO OBSTACLES DISPLAYED

OFF

SAFE, CAUTION, AND WARNING OBSTACLES
DISPLAYED

OFF

CAUTION AND WARNING OBSTACLES
DISPLAYED

SAFE, CAUTION, AND WARNING OBSTACLES
DISPLAYED

Note: Obstacles are only displayed at certain map
zoom ranges, on certain map ﬁelds, and will only
be displayed if an obstacle database is loaded
on the SD card.
Note: The table above is only for the Navigation
Map Page. The Terrain Proximity Page always
shows ONLY caution and warning obstacles.

Obstacle Shapes
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)

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SECTION 4 – MFD

4.8 DIRECT-TO NAVIGATION

To select a direct-to destination:

The “Direct-to” function provides a quick method of
setting a course to a destination waypoint. Once a Direct-to is activated, the G1000 establishes a point-to-point
course line from the present position to the selected Direct-to destination. If the course change is greater than
30 degrees, a course extension is offset from the present
position to allow a standard rate turn to intercept the Direct-to course line. Note that the CDI (HSI) needle will
not be immediately centered in this case. Direct-to course
guidance is provided until the Direct-to is cancelled or
replaced by a new destination, and the navigation data is
displayed on the Navigation Map Page.

Identiﬁer
Facility Name
City

Symbol
Nearest Airport
Selection

Flight Plan Waypoint Selection

Map Orientation

Press the Direct-to key. The Direct-to page
is displayed with the destination ﬁeld highlighted.

Turn the small FMS knob to enter the ﬁrst letter
of the destination waypoint identiﬁer. The
destination waypoint may be an airport, VOR,
NDB, intersection or user waypoint, as long as
it is in the database or stored in memory as a
user waypoint. Turn the large FMS knob to the
right to move the cursor to the next character
position.

Repeat steps 2 and 3 to spell out the rest of
the waypoint identiﬁer.

Press the ENT key to conﬁrm the identiﬁer. The
‘Activate?’ ﬁeld is highlighted.

Press the ENT key to activate a Direct-to course
to the selected destination.

If navigating to a waypoint and the aircraft moves off
course, the direct-to feature can be used to re-center the
CDI (HSI) needle and proceed to the same waypoint.
To re-center the CDI (HSI) needle to the
same destination waypoint:

Map of the
Selected
Waypoint
Map Range
Bearing
Distance

Region
Latitude/
Longitude

Direct-to
Course

Activate Field

Press the Direct-to key, followed by pressing the ENT key twice. NOTE: If navigating
an approach with the missed approach point
(MAP) as the current destination, re-centering
the CDI (HSI) needle with the Direct-to key
cancels the approach.

Figure 4-18 Direct-to Page

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SECTION 4 – MFD

Direct to Navigation Operations

Continue turning the small FMS knob to scroll
through any additional database listings for
the selected facility name or city. The small
FMS knob can be used to scroll backwards if
the desired waypoint was passed up.

Press the ENT key to conﬁrm the selected waypoint, and ENT again to activate a Direct-to.

Selecting a Direct-to Waypoint
In addition to selecting a Direct-to waypoint using an
identiﬁer, a Direct-to waypoint can be selected in the following ways:
• by facility or city name
• from the active ﬂight plan
• from the nearest airports list
• from a waypoint ﬁeld, waypoint page, or map
highlight shortcut
Selecting a Direct-to Destination by Facility or City
Name

Selecting a Direct-to Destination from the Active
Flight Plan
Any waypoint contained in the ﬂight plan may be selected as a direct-to destination from the Direct-to Waypoint Page when navigating an active ﬂight plan.

In addition to selecting a destination by identiﬁer, the
Direct-to Page also allows the selection of airports, VORs
and NDBs by facility or city name. If duplicate entries
exist for the entered facility or city name, additional entries can be viewed by continuing to turn the small FMS
knob during the selection process.
To select a direct-to destination by facility
name or city:
1.

Press the Direct-to key. The Direct-to Page is
displayed with the waypoint identiﬁer ﬁeld
highlighted.

Turn the large FMS knob to highlight the facility
or city name ﬁeld.

Turn the small and large FMS knob to enter
the facility or city location of the desired waypoint.
NOTE: the G1000s Spell N Find feature selects
the ﬁrst entry in the database based on the characters that have been entered to that point.

Figure 4-19 Flight Plan Waypoint Direct-to

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SECTION 4 – MFD
To select a Direct-to destination from the
active ﬂight plan:
1.

Press the Direct-to key. The Direct-to Waypoint
Page is displayed with the waypoint identiﬁer
ﬁeld highlighted.

Turn the large FMS knob to highlight the ﬂight
plan ‘FPL’ ﬁeld.

Turn the small FMS knob to display a window
showing all waypoints in the active flight
plan.

Continue turning the small FMS knob to scroll
through the list and highlight the desired
waypoint.

Press the ENT key to conﬁrm the selected waypoint, and ENT again to activate a Direct-to.

Selecting a Nearest Airport as a Direct-to
Destination
The Direct-to Page always displays the nearest airports
(from the present position) on the NRST ﬁeld.
To select a nearby airport as a direct-to
destination:

Press the Direct-to key. The Direct-to Page
appears with the destination field highlighted.

Turn the large FMS knob to highlight the nearest airport ﬁeld.

Turn the small FMS knob to display a window
showing up to nine nearby airports. Continue
turning the small FMS knob to scroll through
the list and highlight the desired airport.

Press the ENT key to conﬁrm the selected waypoint, and ENT again to activate direct-to.

Shortcuts
Shortcuts are available when using the Direct-to key,
allowing the pilot to bypass the use of the small and large
FMS knobs. Any time a waypoint ﬁeld is highlighted and
then the Direct-to key is pressed, the highlighted waypoint will be the direct-to waypoint.

The following are “candidates” for Direct-to waypoints:
• The highlighted waypoint when map panning
with the MFD map panning pointer.
• The highlighted waypoint identiﬁer ﬁeld on any
page.
• The airport waypoint page airport when on
the airport information, arrival, departure, or
approach pages.
• The waypoint displayed on the VOR waypoint
page.
• The waypoint displayed on the NDB waypoint
page.
• The waypoint displayed on the intersection waypoint page.
• The waypoint displayed on the user waypoint
page.

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SECTION 4 – MFD
Canceling Direct-to Navigation
Once a direct-to is activated, the G1000 provides
navigation guidance to the selected destination until the
direct-to is either replaced with a new direct-to or ﬂight
plan, or cancelled, or if the unit is turned off.
To cancel a direct-to:
1.

Press the Direct-to key to display the Direct-to
Page.

Press the MENU key to display the direct-to
options menu.

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.

Figure 4-20 Nearest Airport Direct-to

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SECTION 4 – MFD
Specifying a Course to a Waypoint
When Direct-to is activated, the G1000 sets a direct
great circle course to the selected destination. The course
to the destination, using the course ﬁeld on the Direct-to
Page can be manually deﬁned.
To manually deﬁne the direct-to course:

Press the Direct-to key.

Turn the small and large FMS knobs to select
the destination waypoint.

Press the ENT key to conﬁrm the selected waypoint, then turn the large FMS knob to highlight
the course ﬁeld.

Turn the small and large FMS knobs to select
the desired course and press the ENT key.

Press the ENT key again to begin navigation
using the selected destination and course.

Figure 4-21 Manual Course Direct-to

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SECTION 4 – MFD

4.9 FLIGHT PLANS
The G1000 can create up to 99 different ﬂight plans
with up to 31 waypoints in each ﬂight plan. The ﬂight
plan (FPL) page group consists of three pages:
• Active Flight Plan
• Flight Plan Catalog
• Vertical Navigation
The Flight Plan Pages are used to create, edit and copy
ﬂight plans. The Vertical Navigation Page is used to create
a three-dimensional proﬁle which guides the aircraft to a
ﬁnal (target) altitude at a speciﬁed location.

Active Flight Plan Page
The Active Flight Plan Page provides information and
editing functions for the ﬂight plan currently in use for
navigation. Once a Direct-to or ﬂight plan has been activated, the Active Flight Plan Page shows the following:
• Each waypoint for the ﬂight plan (or a single waypoint for a Direct-to), along with the desired track
(DTK) and distance of each leg (DIS).
• Active leg information with enroute safe altitude
(ESA) for the speciﬁed leg.
• Active FPL information with enroute safe altitude
(ESA)
• Flight plan information showing remaining leg
and remaining total distance, and enroute safe
altitude for the entire route.

The data ﬁelds are user-selectable and can be changed
to display the following:
•
•
•
•
•
•

Cumulative Distance (CUM)
Distance (DIS)
Desired Track (DTK)
Enroute Safe Altitude (ESA)
Estimated Time of Arrival (ETA)
Estimated Time Enroute (ETE)

Active Flight Plan Page Operations
The following options are available for the Flight Plan
Page:
•
•
•
•
•
•
•
•
•
•
•
•
•

Activate Leg
Store Flight Plan
Invert Flight Plan
Delete Flight Plan
Load Departure
Load Arrival
Load Approach
Remove Arrival
Remove Departure
Remove Approach
Closest Point of FPL
Change Fields
Restore Defaults

Create a New Flight Plan
‘Create New Flight Plan’ creates a new ﬂight plan.
To create a new ﬂight plan:
1.

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Press the MENU key to display the Flight Plan
Catalog Page options.

Turn the large FMS knob to highlight ‘Create
New Flight Plan’ and press the ENT key.

A blank ﬂight plan page appears for the ﬁrst

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SECTION 4 – MFD
empty storage location. Turn the small and
large FMS knobs to enter the identiﬁer of the
departure waypoint and press the ENT key.
5.

Repeat step number 4 to enter the identiﬁer
for each additional ﬂight plan waypoint.

Once all waypoints have been entered, press
the FMS knob to return to the Flight Plan
Catalog Page.

Figure 4-22 New Flight Plan

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SECTION 4 – MFD
To edit a ﬂight plan:
1.

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Press the FMS knob to activate the cursor.

Turn the large FMS knob to highlight the
desired ﬂight plan and press the ENT key.

To add a waypoint to the ﬂight plan: Turn the
large FMS knob to select the point where the
new waypoint is to be added. (If an existing
waypoint is highlighted, the new waypoint is
placed directly in front of this waypoint.) Turn
the small and large FMS knobs to enter the
identiﬁer of the new waypoint and press the
ENT key.

To delete a waypoint from the ﬂight plan: Turn
the large FMS knob to select the waypoint
to delete and press the CLR key to display a
remove waypoint conﬁrmation window. With
‘OK’ highlighted, press the ENT key to remove
the waypoint. To cancel, turn the large FMS
knob to highlight ‘CANCEL’ and press the ENT
key.
Once all changes have been made, press the
FMS knob to return to the Flight Plan Catalog
Page.

Delete a Waypoint
To delete a waypoint from an existing ﬂight
plan:
1.

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Press the FMS knob to activate the cursor.

Turn the large FMS knob to highlight the
desired ﬂight plan and press the ENT key.

Turn the large FMS knob to select the waypoint
to delete and press the CLR key to display a
‘REMOVE WAYPOINT’ conﬁrmation window.

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.

Once all changes have been made, press the
FMS knob to return to the Flight Plan Page.

Figure 4-23 Remove Waypoint Conﬁrmation

Remove Departure, Arrival, or Approach
• ‘Remove Departure’ deletes the current DP from
the active ﬂight plan.
• ‘Remove Arrival’ deletes the current STAR from
the active ﬂight plan.
• ‘Remove Approach’ deletes the currently selected
approach from the active ﬂight plan.

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SECTION 4 – MFD
To remove an approach, arrival or departure from the active ﬂight plan:
1.

From the Active Flight Plan Page, press the
MENU key to display the Active Flight Plan Page
options.

Select the ‘Remove Approach’, ‘Remove Arrival’
or ‘Remove Departure’ option and press the
ENT key.

A conﬁrmation window is displayed listing the
procedure the pilot is about to remove. With
‘OK’ highlighted, press the ENT key. To cancel
the remove request, turn the large FMS knob
to highlight ‘CANCEL’ and press the ENT key.

FLIGHT PLAN CATALOG PAGE
The Flight Plan Catalog Page is the second ﬂight planning
page and provides ﬂight planning information and editing
capability. Once a Direct-to or ﬂight plan has been
activated, the Flight Plan catalog Page displays the following:
• Number of ﬂight plans in memory.
• Flight Plan List.
• Flight Plan information box containing departure, destination, total distance, and enroute safe
altitude information.
To display the Flight Plan Catalog Page:
1.

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Flight Plans
in Memory
Flight Plan List

Figure 4-24 Removing an Approach

Flight Plan
Information

Figure 4-25 Flight Plan Catalog Page

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SECTION 4 – MFD
Flight Plan Catalog Page Operations
The following operations can be performed from the
Flight Plan Catalog Page:
•
•
•
•
•
•
•
•
•
•

Activate a Flight Plan
Stop Navigating a Flight Plan
Invert and Activate a FPL
Create a New Flight Plan
Copy a Flight Plan
Delete a Flight Plan
Delete All Flight Plans
Sort Flight Plans by Comment
Flight Plan Catalog Page Options
Edit a Flight Plan

desired ﬂight plan and press the MENU key to
display the Flight Plan Catalog Page options.
4.

Turn the large FMS knob to highlight ‘Activate
Flight Plan’ and press the ENT key.

An ‘Activate stored ﬂight plan?’ conﬁrmation
window is displayed. 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.

Figure 4-27 Activate Stored Flight Plan Conﬁrmation

Stop Navigating a Flight Plan
To stop navigating a ﬂight plan:

Figure 4-26 Flight Plan Catalog Page Options

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Press the FMS knob to activate the cursor.

Turn the large FMS knob to highlight the
desired ﬂight plan and press the MENU key to
display the Flight Plan Catalog Page options.

Turn either the small or large FMS knob to
highlight ‘Delete Flight Plan’ and press the ENT
key. A ‘Delete Flight Plan’ conﬁrmation window
is displayed. With ‘OK’ highlighted, press the
ENT key to delete the ﬂight plan. To cancel the
ﬂight plan deletion, turn the large FMS knob
to highlight ‘CANCEL’ and press the ENT key.

Activate a Flight Plan
Once a ﬂight plan is deﬁned using the Flight Plan
Catalog Page it can be activated for navigation. Activating
the ﬂight plan overwrites any previous information at that
location.
To activate (begin to navigate) an existing
ﬂight plan:
1.

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Press the FMS knob to activate the cursor.

Turn the large FMS knob to highlight the
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
To copy a ﬂight plan to another ﬂight plan
catalog location:
1.

From the Flight Plan Catalog press the FMS
knob to activate the cursor, turn the large
FMS knob to highlight the ﬂight plan the pilot
wishes to copy, then press the MENU key to
display the Flight Plan Catalog Options.

Turn the large FMS knob to highlight ‘Copy
Flight Plan’ and press the ENT key.

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 4-28 Delete Flight Plan Conﬁrmation

Invert and Activate a Flight Plan
‘Invert & Activate FPL’ allows the active ﬂight plan to
be inverted and activated for navigation.
To invert and activate a ﬂight plan:
1.

Press the FPL key and turn the small FMS knob
to display the Flight Plan Catalog Page.

Press the FMS knob to activate the cursor.

Turn the large FMS knob to highlight the
desired ﬂight plan and press the MENU key to
display the Flight Plan Catalog Page options.

Turn either the small or large FMS knob to
highlight ‘Invert & Activate FPL’ and press the
ENT key.

An ‘Invert and activate stored ﬂight plan?’
confirmation window is displayed. With
‘OK’ highlighted, press the ENT key to inverts
and activate the ﬂight plan. To cancel the
operation, turn the large FMS knob to highlight
‘CANCEL’ and press the ENT key.

Delete a Flight Plan
‘Delete Flight Plan’ removes all waypoints from the
active ﬂight plan. (Deleting a ﬂight plan does not delete
the waypoints contained in the ﬂight plan from the database or user waypoint memory.) Once the pilot is ﬁnished
with a ﬂight plan, it can easily be deleted from the Flight
Plan Catalog Page or the Active Flight Plan Page.
To delete a ﬂight plan from the Active
Flight Plan Page:
1.

From the Active Flight Plan Page, press the
MENU key to display the Active Flight Plan
options window.

Turn the large FMS knob to highlight ‘Delete
Flight Plan’ and press the ENT key.

A ‘Delete all waypoints in ﬂight plan?’ conﬁrmation window is displayed. With ‘OK’ highlighted, press the ENT key to delete the active
ﬂight plan. To cancel, turn the large FMS knob
to highlight ‘CANCEL’ and press the ENT key.

Copy a Flight Plan
‘Copy Flight Plan’ copies the active ﬂight plan to a
Flight Plan Catalog location. The copy function is useful for duplicating the active ﬂight plan before making
changes.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
To delete a ﬂight plan from the Flight Plan
Catalog Page:
1.

From the Flight Plan Catalog Page, press the
FMS knob to activate the cursor, turn the
large FMS knob to highlight the ﬂight plan to
delete.

Press the MENU key to display the Flight Plan
Catalog options.

Turn the large FMS knob to highlight ‘Delete
Flight Plan’ and press the ENT key.

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.

Delete All Flight Plans
‘Delete All’ removes all ﬂight plans from memory at
one time.

Point-n-Shoot Flight Plan Creation Feature
The “Point-n-Shoot” ﬂight plan creation feature is activated using the Navigation Map Page and the Active Flight
Plan Page.
1.

Push the Joystick to turn the map cursor on.

Select the Active Flight Plan Page and press
the FMS knob to highlight the list of waypoints.
Waypoints will be inserted ABOVE the highlighted row if the cursor is on. Waypoints will
be inserted at the END of the ﬂight plan if the
cursor is off.

To insert waypoints, use the map cursor to
point at the desired waypoint (it will become
visually enhanced when it is properly pointed
to), and press the LD WPT softkey. Existing user
waypoints are inserted in the same manner.

If the selected waypoint is not a Jeppesen
waypoint (Airport or Navaid) or user waypoint,
the G1000 creates a user waypoint (beginning
with ‘USR000’) at the point and inserts it into
the ﬂight plan.

The pilot can also create and insert a user
waypoint by pointing at a blank spot on the
nav map and pressing ‘LD WPT’. This creates
a user waypoint at the map cursor and inserts
it into the ﬂight plan.

To delete all ﬂight plans:
1.

From the Flight Plan Catalog Page, press the
MENU key to display the Flight Plan Catalog
Page options.
Turn the large FMS knob to highlight ‘Delete
All’ and press the ENT key. A ‘Delete all ﬂight
plans?’ confirmation window is displayed.
With ‘OK’ highlighted, press the ENT key to
delete all ﬂight plans. To cancel, turn the large
FMS knob to highlight ‘CANCEL’ and press the
ENT key.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

4.10 PROCEDURES

To select a departure:

Arrivals and Departures
Based upon the active ﬂight plan or Direct-to destination, the Procedures Page provides direct access to approaches, departures and arrivals. The Procedures Page is
displayed by pressing the PROC key.

Press the PROC key. Turn the large FMS knob
to highlight ‘Select Departure’ and press the
ENT key. The departure procedure window
appears.
Turn the FMS knob to select the desired departure and press the ENT key. The transition
window appears.
Turn the FMS knob to select the desired
transition and press the ENT key. ‘LOAD?’ is
highlighted. Press the ENT key.
NOTE: Vector departures are not part of the
aviation database.

To select an arrival:
1.

Press the PROC key. Turn the large FMS knob
to highlight ‘Select Arrival’ and press the ENT
key. The arrival procedure window appears.

Turn the FMS knob to enter the desired arrival
and press the ENT key. The transition window
appears.
NOTE: The approach vectors option assumes
the pilot will receive vectors to the ﬁnal course
segment of the approach and will provide navigation guidance on the ﬁnal approach segment
and extension only.

Figure 4-29 Procedures Page

NOTE: Pilots should be familiar with section
1-1-20 of the Aeronautical Information Manual
(AIM) regarding the use of GPS.

Turn the FMS knob to select the desired
transition and press the ENT key. ‘LOAD?’ is
highlighted. Press the ENT key. Review the
ﬂight plan for accuracy. If the destination is
listed twice, remove the ﬁrst one if the arrival
is ﬁled as part of the ﬂight plan. If the arrival
is received enroute, highlight the ﬁrst point of
the arrival, press direct-to, and enter when the
clearance is received. Sequencing is automatic
thereafter.

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SECTION 4 – MFD

Approaches
The G1000 allows you to ﬂy non-precision and precision approaches to airports with published instrument
approach procedures. All available approaches are part of
the Jeppesen database stored internally in each PFD and
MFD.
The G1000 provides both lateral and vertical guidance
for ILS precision approaches on the PFD, and lateral guidance for non-precision Localizer, GPS, and VOR and ADF
overlay approaches. GPS position information is also provided on the mapping portion of the MFD and the inset
map window on the PFD for pilot reference only.
G1000 Navigational Guidance for Approaches
The G1000 supports all ARINC 424 leg types that have
associated waypoint ﬁxes. The G1000 uses the following
leg types as part of the Jeppesen database:
•
•
•
•
•
•
•
•
•
•
•
•
•
•

AF - DME arc to a ﬁx
CF – Course to a ﬁx
DF – Direct to a ﬁx
FA – Course from ﬁx to an altitude
FC – Course from ﬁx to distance
FD – Course from ﬁx to DME distance
FM – Course from ﬁx to manual termination
HA – Hold terminating at altitude
HF – Hold terminating at a ﬁx
HM – Hold with manual termination
IF – Initial ﬁx
PI – Procedure turn to course intercept
RF – Constant radius turn to ﬁx
TF – Track between two ﬁxes

Each of these legs is displayed on the active ﬂight plan.
The G1000 does not support the following legs:
•
•
•
•
•
•
•
•
•

CA – Course to an altitude
CD – Course to a DME distance
CI – Course to an intercept
CR – Course to a radial
VA – Heading vector to an altitude
VD – Heading vector to DME distance
VI – Heading vector to an intercept
VM – Heading vector to manual termination
VR – Heading vector to a radial

NOTE: The G1000 does not provide steering guidance for hold legs and procedure turns (HA, HF,
HM and PI leg types). However, these legs are
drawn on the map and are shown in the ﬂight
plan.
NOTE: The pilot is responsible for determining
database currency for approaches.
NOTE: The approach charts shown in this section
are not drawn to range and are not to be used
for navigation.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

Selecting Approaches
In order to select an approach, there must be an active
ﬂight plan or direct-to which terminates at an airport with
a published approach.
To select an approach:
1.

Press the PROC key to display the Procedures
Page. Turn the large FMS knob to highlight
‘Select Approach’ and press the ENT key. The
approach procedure window appears.

Turn the FMS knob to select the desired
approach and press the ENT key. The transition
window appears.
NOTE: The approach vectors option assumes
the pilot will receive vectors to the ﬁnal course
segment of the approach and will provide navigation guidance on the ﬁnal approach segment
and extension only.

Figure 4-30 Selecting an Approach Procedure

Turn the FMS knob to select the desired transition and press the ENT key. ‘LOAD?’ is now
highlighted. Press the ENT key. Activate the
approach once the approach clearance is
received.
NOTE: ‘LOAD?’ will add the procedure to the
flight plan without immediately using it for
navigation guidance. This allows you to continue
navigating the original ﬂight plan, but keeps the
procedure available on the Active Flight Plan
Page for quick activation when needed. ‘Activate?’ overrides the enroute portion of the active
ﬂight plan, proceeding directly to the approach
portion.
NOTE: You can also load an approach by pressing
the APR softkey.

Figure 4-31 Selecting an Approach Transition

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Not all approaches in the database are approved for
GPS use. As you select an approach, a ‘GPS’ designation
to the right of the procedure name indicates the procedure
can be ﬂown using the GPS receiver. Some procedures
will 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,
you must use the appropriate receiver 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.
A selected approach can be activated or loaded. Activating the approach also initiates automatic CDI scaling
transition as the approach progresses. In many cases, it
can be easiest to “Load” the full approach while still some
distance away, enroute to the destination airport. Later,
if vectored to ﬁnal, use the following steps to select ‘Activate Vector-To-Final’ – which makes the inbound course
to the FAF waypoint active. Otherwise, activate the full
approach using the ‘Activate Approach?’ option.

To activate an Approach Procedure:
1.

With an approach loaded in the active ﬂight
plan, press the PROC key to display the Procedures Page.

Turn the large FMS knob to highlight ‘Activate
Approach’.

Press the ENT key.

Figure 4-32 Activating an Approach Procedure

CAUTION: The G1000 is designed to complement
the printed approach charts and vastly improve
situational awareness throughout the approach.
The approach must be ﬂown as it appears on the
approach chart.

NOTE: The GPS approach examples given in
the next section are not to be used for navigation. They are to be used in conjunction with
the G1000 PC training simulator software for
practice in learning what types of approaches
the G1000 supports

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

GPS Approach Examples
No Procedure Turn
An approach where there is no procedure turn required to get established on the inbound course to the
FAF is our example. GPS RWY 12 is used to show how
the G1000 sequences through an approach and what type
of annunciation and range factor changes can be expected
(the G1000 automatically sequences through all legs of an
approach without pilot input other than to activate the approach and to sequence past the missed approach point).
This example is based upon and active ﬂight plan from
KFLG (Flagstaff, AZ Pulliam Airport) to KPRC (Prescott,
AZ Love Airport).
1.
2.

Select KPRC as the destination, via the Direct-to
key or as the last waypoint in a ﬂight plan.
Press the PROC key and select the GPS RWY 12
approach. From the transitions window, select
IRODY as the IAF (select ‘LOAD?’).
Within 30 nm of the destination, the G1000
switches from enroute mode to terminal mode.
The switch to terminal mode is accompanied
by a gradual CDI scale transition from 5.0 to
1.0 nm full scale deﬂection.
Prior to reaching the IAF (IRODY), the approach
sequence should be reviewed. Press the FPL
key to display the Active Flight Plan Page. Press
the FMS knob and turn the large FMS knob to
review each segment of the approach. When
ﬁnished press the FPL key again to return to
the previous page.
As the pilot approaches the IAF (IRODY), a
waypoint message ‘NEXT DTK 204°’ appears
in the navigation status bar on the PFD. As
the distance to the IAF approaches zero, the
message is replaced by a turn advisory ‘TURN
TO 204°’.

As the pilot approaches the IAP (OKAPY), a
waypoint message ‘NEXT DTK 124°’ appears.
As the distance approaches zero the message is
replaced by a turn advisory ‘TURN TO 124°’.

At 2.0 nm from the FAF (MULHU), the G1000
switches from terminal mode to approach
mode. CDI scaling begins rounding down from
1.0 to 0.3 nm full scale deﬂection.

Upon crossing the FAF ‘NEXT DTK 124°’
appears and the destination sequences to the
MAP (RW12map, the runway threshold). Keeping the needle centered, ﬂy toward the MAP,
observing the altitude minimums dictated by
the approach plate.

As the pilot approaches the MAP, a waypoint
message ‘ARRIVING AT WAYPOINT’ appears.

10. Upon crossing the MAP, ‘SUSP’ appears on the
HSI and directly above the SUSP softkey, indicating that automatic sequencing of approach
waypoints is suspended at the MAP. A ‘FROM’
indication is displayed on the CDI, but course
guidance along the final approach course
continues. If a missed approach is required,
use the SUSP softkey to initiate the missed
approach sequence.
NOTE: When the message ‘RAIM is not available’ appears in the Alerts Window on the PFD
a missed approach must be executed. Refer to
section 1-1-20 in the Aeronautical Information
Manual (AIM) for information regarding RAIM.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.

SECTION 4 – MFD

Figure 4-33 Approach with No Procedure Turn

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Flying the Missed Approach
As you pass the MAP, and the runway is not in view, a
missed approach must be performed. The G1000 continues to give guidance along an extension of the ﬁnal course
segment (FAF to MAP) until you manually initiate the
missed approach procedure.

Upon crossing the MAP, a waypoint message
‘ARRIVING AT WAYPOINT’ appears in the
navigation status bar on the PFD. ‘SUSP’
appears on the HSI and directly above the OBS
softkey, indicating that automatic sequencing
of approach waypoints is suspended. A ‘FROM’
indication is displayed on the CDI, however
course guidance along the final approach
course continues. Use the SUSP softkey to
initiate the missed approach sequence. Be
sure to follow the published procedure. If a
runway heading is prescribed by ATC the pilot
must not press the SUSP softkey until they are
ready to turn. Press the CDI softkey to resume
GPS navigation.

Press the SUSP softkey. The missed approach
holding point (IRODY) is automatically offered
as the destination waypoint.

Follow the missed approach procedures, as
dictated by the approach chart. The G1000
gives guidance to the holding point.

A message appears in the navigation status bar
on the PFD recommending entry procedures for
the holding pattern ‘HOLD PARALLEL’.

The G1000 provides course guidance only
on the inbound side of the holding pattern.
When leaving the holding pattern to re-ﬂy
the approach, press the PROC key to ‘Select
Approach?’ or ‘Activate Approach?’ (or add a
new destination to the ﬂight plan).

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.

SECTION 4 – MFD

Figure 4-34 Flying the Missed Approach

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Flying the Procedure Turn
The procedure turn portion of the approach is stored
as one of the legs of the approach. For this reason the
G1000 requires no special operations from the pilot (other than ﬂying the procedure turn itself) beyond what is
required for any other type of approach. This example
is based upon a ﬂight from KILG (Wilmington, DE New
Castle County) to KMIV (Millville, NJ Municipal). The
approach into KMIV will be NDB or GPS RWY 14 with
the RNB transition.
1.

Select KMIV as the destination.

Press the PROC key and select the NDB or
GPS RWY 14 approach. From the transitions
window select RNB as the IAF. Load the procedure.

When cleared for the approach, press the PROC
key and select ‘ACTIVATE APPROACH?’.

Within 30 nm of the destination, the G1000
switches from enroute mode to terminal mode.
The switch to terminal mode is accompanied
by a gradual scale transition from 5.0 to 1.0
nm, full scale deﬂection.

Prior to reaching the IAF (RNB), you may wish
to review the approach sequence. Press the FPL
key to display the Active Flight Plan Page. Press
the FMS knob and turn the large FMS knob to
review each segment of the approach. When
ﬁnished, press the FPL key again to return to
the previous page.
As the pilot approaches the IAF (RNB), a
waypoint message ‘NEXT DTK 327°’ appears
in the navigation status bar on the PFD. As
the distance approaches zero the message is
replaced by a turn advisory ‘TURN TO 327°’.

Fly the outbound course keeping the CDI needle
centered.

After ﬂying approximately one minute past
the IAF, the message ‘START PROC TURN’
appears.

Turn left to a heading of 282° to initiate the
procedure turn. No guidance through the
procedure turn is given. The procedure turn is
displayed in magenta indicating the active leg.
The CDI needle starts moving to the right.

10. After approximately one minute, make a 180°
right turn to a heading of 102° to intercept the
inbound course. The G1000 sequences to the
inbound leg to the FAF, the CDI needle swings
to the opposite side to provide proper sensing
along the ﬁnal course segment and ‘NEXT DTK
147°’ appears in the navigation status bar on
the PFD.
11. As the CDI needle starts to center, make a right
turn to 147° to intercept the ﬁnal approach
course.
12. At 2.0 nm from the FAF (RNB), the G1000
switches from terminal mode to approach
mode. CDI scaling begins rounding down from
1.0 to 0.3 nm, full scale deﬂection.
13. Upon crossing the FAF, the message ‘NEXT DTK
147°’ appears and the destination sequences
to the MAP (RW14map, the runway threshold).
Keeping the CDI needle centered, ﬂy toward
the MAP, observing the altitude minimums
dictated by the approach chart.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
14. As the pilot approaches the MAP, a waypoint
message ‘ARRIVING AT WAYPOINT’ appears.

Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.

15. Upon crossing the MAP, ‘SUSP’ appears on the
HSI and directly above the SUSP softkey, indicating that automatic sequencing of approach
waypoints is suspended. A ‘FROM’ indication
is displayed in the CDI, but course guidance
along the ﬁnal approach course continues.
If a missed approach is required, use the
SUSP softkey to initiate the missed approach
sequence.

NOTE: Once you cross the FAF, the ﬁnal course
segment is displayed in magenta and a dashed
line extends the course beyond the missed
approach point. The dashed line is provided for
situational awareness only and should NOT be
used for navigation. Follow the published missed
approach procedures.

Figure 4-35 Flying the Procedure Turn

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SECTION 4 – MFD
Flying the DME ARC
The GPS overlay for a DME arc approach uses additional Jeppesen provided waypoints to deﬁne the arc.
When cleared for a DME arc approach, you may do either
of the following to intercept the arc:

Follow the arc, keeping the CDI needle centered.

The next point in the approach is an intermediate ﬁx “WILDE”. As you approach “WILDE” a
waypoint message ‘NEXT DTK 072°’ appears.
As the distance to this ﬁx approaches zero the
message is replaced by a turn advisory ‘TURN
TO 072°’. Initiate a standard rate turn to this
course heading.

At 2.0 nm from the FAF (PINTO), the G1000
switches from terminal mode to approach
mode. CDI scaling begins rounding down from
1.0 to 0.3 nm, full scale deﬂection.

As the pilot approaches the FAF, a waypoint
message ‘NEXT DTK 072°’ appears. Make
any adjustments necessary for the ﬁnal course
segment (FAF to MAP).

• Proceed direct to the IAF.
• Follow ATC vectors, which allow you to intercept
the arc at any point along the arc.
This example is based upon a ﬂight from KSAF (Santa
Fe, NM Municipal) to KFMN (Farmington, NM Four
Corners Regional). The VOR DME RWY 7 approach is
selected along with “HIDOX” as the IAF.

Select KFMN as your destination.

Press the PROC key and select the ‘VOR DMW
RWY 7’ approach. From the transitions
window, select “HIDOX” as the IAF. Load the
procedure.

Within 30 nm of KFMN, the G1000 switches
from enroute mode to terminal mode. The CDI
scale gradually transitions from 5.0 to 1.0 nm,
full scale deﬂection.

Activated the approach when cleared by ATC.

As the pilot approaches the IAF (HIDOX), a
waypoint message ‘NEXT DTK 206°’ appears
in the navigation status bar on the PFD. As
the distance to the IAF approaches zero, the
message is replaced by a turn advisory ‘TURN
TO 206°’.

10. Upon crossing the FAF, the destination
sequences to the MAP (RW07map, the runway
threshold). Keeping the CDI needle centered,
ﬂy toward the MAP, observing the altitude
minimums dictated by the approach plate.
11. As the pilot approaches the MAP, a waypoint
message ‘ARRIVING AT WAYPOINT’ appears.
12. Upon crossing the MAP, ‘SUSP’ appears on the
HSI and directly above the SUSP softkey, indicating that automatic sequencing of approach
waypoints is suspended. A ‘FROM’ indication is
displayed on the CDI, however course guidance
along the ﬁnal approach course continues. If
a missed approach is required, use the SUSP
softkey to initiate the missed approach.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.

SECTION 4 – MFD

Figure 4-36 Flying the DME Arc and Vectors to the DME Arc

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD
Flying a Holding Pattern
This example is based upon a missed approach from
KSOP (Moore County, NC). Now you’ve decided to divert
to KIGX (Chapel Hill, NC) instead. You select the RNAV
(GPS) RWY 9 approach into KIGX. The RNAV (GPS)
RWY 9 approach begins with a holding pattern at the IAF,
FIKKA.
1.

From the Active Flight Plan Page highlight KIGX
and press the Direct-to key, then press the ENT
key twice.

Press the PROC key and select the RNAV (GPS)
RWY 9 approach.

From the transitions window, select FIKKA as
the IAF, then you will be asked ‘Hold at FIKKA?’
Select Yes or No and press the ENT key. Choose
‘ACTIVATE?’, this will load and activate the
approach.

Upon activating the approach, the Active Flight
Plan Page appears. Review the approach
sequence by pressing the small FMS knob and
turning the large FMS knob to review each
segment of the approach.

Within 30 nm of the airport, the G1000
switches from enroute mode to terminal mode.
The CDI scale transitions from 5.0 to 1.0 nm,
full scale deﬂection.

Prior to crossing FIKKA, a message ‘HOLD
DIRECT’ appears in the navigation status bar
on the PFD to suggest the proper holding pattern entry.

Fly the holding pattern (the holding pattern
is displayed in magenta, indicating the active
leg).

Upon crossing the IAF, ‘SUSP’ appears on the
HSI and directly above the OBS softkey indicating that automatic sequencing of approach
waypoints is suspended. As the pilot makes
the turn inbound, ‘SUSP’ is cancelled and the
G1000 returns to automatic sequencing.

As the pilot approaches FIKKA from within the
holding pattern, a waypoint message (NEXT
DTK 090°) appears.

10. At 2.0 nm from the FAF, the G1000 switches
from terminal mode to approach mode. CDI
scaling begins rounding down from 1.0 to 0.3
nm, full scale deﬂection.
11. As the pilot approaches the FAF, a waypoint
message (NEXT DTK 090°) appears. Make
any course adjustments necessary for the ﬁnal
course segment (FAF to MAP).
12. Upon crossing the FAF, the destination
sequences to the MAP (RW09map, the runway
threshold). Keeping the needle centered ﬂy
toward the MAP, observing the altitude minimums dictated by the approach chart.
NOTE: When viewing the Navigation Map Page,
the ﬁnal course segment is displayed in magenta
(the active leg of the ﬂight plan always appears
in magenta) and a dashed line extends the course
beyond the MAP. Do NOT follow this extended
course. Instead, follow the published missed
approach procedures.

13. As the pilot approaches the MAP, a waypoint
message ‘ARRIVING AT WAYPOINT’ appears.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

NOTE: Remember do not press the OBS softkey
until you are ready to make the turn.

Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.

14. Upon crossing the MAP, ‘SUSP’ appears on the
HSI and directly above the SUSP softkey, indicating that automatic sequencing of approach
waypoints is suspended at the MAP. A ‘FROM’
indication is displayed on the CDI, however
course guidance along the final approach
course continues. If a missed approach is
required, use the SUSP softkey to initiate the
missed approach sequence.

Figure 4-37 Flying a Holding Pattern

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 4 – MFD

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Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

A.1 INTRODUCTION
IMPORTANT NOTE: The Aircraft Flight Manual
takes precedence over any conﬂicting information found in Appendix A.

• Audio Alerting System: The G1000 system
issues audio alert sounds and aural voice messages
when speciﬁc system conditions are met. See Section A.3 for more information.

The G1000 Alerting System conveys alerts to the pilot
using a combination of the following items:
• Annunciation Window: The Annunciation
Window is not used for Mooney aircraft. It is
shown for pilot awareness of the system.

System
Annunciation
Red ‘X’

• Alerts Window: The Alerts window displays
alert text messages. Up to 64 prioritized alert text
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 alerts, the
ALERTS softkey may appear as a ﬂashing
annunciation. By pressing the softkey, the pilot
acknowledges awareness of the alert. The pilot
can press the ALERTS softkey a second time to
view alert text messages.

Annunciation
Window
(Not Used By
Mooney)

Alerts Window

Figure A-1 G1000 Alerting System

Softkey
Annunciation

• 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 Section A.4 for more information.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

A.2 ALERT LEVELS
The G1000 Alerting System uses a single alert level for
Mooney aircraft:
• MESSAGE ADVISORY: A Message Advidory alert
is designed to provide general information to the
pilot. This alert is accompanied by a ﬂashing ADVISORY softkey, as shown in Figure A-2. Pressing the
ADVISORY softkey acknowledges the presence of
the alert and displays the alert text message in the
Alerts window. All G1000 system alerts listed in
Section A.5 are categorized as Message Advisories.

Figure A-2 ADVISORY Softkey
Annunciation

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

A.3 MOONEY SPECIFIC AIRCRAFT ALERTS
The following information is conﬁgured speciﬁcally
for the Mooney aircraft. See the Aircraft Flight Manual
and/or Flight Manual Supplement for recommended pilot
actions.

Audio Alerts
Audio Alert

Altitude Alert Chime

Alert Trigger
When aircraft altitude reaches the reference altitude threshold
(+/- 1,000 ft of reference altitude).
When aircraft altitude reaches or goes beyond the reference
altitude deviation limit (+/-200 ft of reference altitude).
When aircraft elevation reaches the reference altitude.

NOTE: Audio and Voice Alerts are provided to
the G1000 by GIA 63 #1. Should this GIA fail,
voice alerts are no longer provided.

Voice Alerts
The following voice alerts can be conﬁgured to be
‘Male’ or ‘Female’ in gender, by going to the AUX-SYSTEM
SETUP Page on the MFD.
Voice Alert

Alert Trigger

“Trafﬁc”

Played when new trafﬁc advisory arrives.

“Trafﬁc Not Available”

Played when the trafﬁc system fails or cannot communicate.
Played when landing gear remain in the ‘Up’ position, and the
pilot retards the throttle to within 1/4” of Idle.
Played when a stall is detected.

“Check Gear”
“Stall”

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

A.4 G1000 SYSTEM ANNUNCIATIONS
When an LRU or an LRU function fails, a large red
‘X’ is typically displayed on windows associated with the
failed data. The following Section describes various system annunciations. Refer to the Aircraft Flight Manual
Supplement and/or Flight Manual Supplement for additional information regarding pilot responses to these annunciations.
System Annunciation

IMPORTANT NOTE: Upon power-up of the
G1000 system, certain windows remain invalid
as G1000 equipment begins to initialize. All
windows should be operational within 1 minute
of power-up. Should any window continue to
remain ﬂagged, have the G1000 system serviced
by a Garmin-authorized repair facility.

Comment

Attitude and Heading Reference System is aligning.

Display system is not receiving attitude information from the AHRS.

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

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

100

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

System Annunciation

Comment

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

Display is not receiving valid heading input from AHRS.

GPS information is either not present or is invalid for navigation use.
Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFMS).

Display is not receiving valid transponder information.
Other Various Red X Indications

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 Mooney M20M & M20R

101

APPENDIX A
A red ‘X’ may be the result of an LRU or an LRU function failure. The ﬁgure presented below illustrates all possible ﬂags and the responsible LRUs.

GIA 63 Integrated
Avionics Units

GIA 63 Integrated
Avionics Units
GDC 74A Air Data
Computer

GRS 77 AHRS
OR
GMU 44
Magnetometer

GEA 71 Engine
Airframe Unit
OR
GIA 63 Integrated
Avionics Unit

GIA 63 Integrated
Avionics Units

GDC 74A Air Data
Computer
Figure A-3 G1000 System Failure Annunciations

102

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

GTX 33 Transponder
OR
GIA 63 Integrated
Avionics Units

APPENDIX A

A.5 G1000 SYSTEM MESSAGE ADVISORIES
This section describes various G1000 system message
advisories. Certain messages are issued due to an LRU or
LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown
in Section A.4.

MFD & PFD Message Advisories

IMPORTANT NOTE: This Section provides information regarding G1000 messages that may be
displayed. 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 Aircraft Flight Manual Supplement and take
precedence over any conﬂicting guidance found
in this Section.

Message
Comments
DATA LOST – Pilot stored data was
Pilot proﬁle data was lost. System reverts to default pilot proﬁle and settings. The
lost. Recheck settings.
pilot may re-conﬁgure the MFD & PFD with preferred settings, if desired.
XTALK ERROR – A ﬂight display
The MFD and PFD are not communicating with each other. Have the G1000 system
crosstalk error has occurred.
serviced.
PFD1 SERVICE – PFD1 needs service.
Return unit for repair.
The PFD and/or MFD self-test has detected a problem. Have the G1000 system
serviced.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
PFD1 CONFIG – PFD1 conﬁguration
error. Conﬁg service req’d.
PFD and/or MFD conﬁguration settings do not match backup conﬁguration memory.
MFD1 CONFIG – MFD1 conﬁguration Have the G1000 system serviced.
error. Conﬁg service req’d.
SW MISMATCH – GDU software
The MFD and PFD have different software versions installed. Have the G1000 system
mismatch. Xtalk is off.
serviced.
MANIFEST – PFD1 software mismatch. Communication halted.
The PFD and/or MFD has incorrect software installed. Have the G1000 system
serviced.
MANIFEST – MFD1 software mismatch. Communication halted.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
The PFD and/or MFD is overheating and is reducing power consumption by dimming
the display. If problem persists, have the G1000 system serviced.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 “KEY” KEYSTK – key is stuck.
A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressMFD1 “KEY” KEYSTK – key is stuck. ing it several times. Have the G1000 system serviced, if the problem persists.
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103

APPENDIX A

Database Message Advisories
Alerts Window Message
Comments
MFD1 DB ERR – MFD1 aviation
database error exists.
The MFD and/or PFD detected a failure in the aviation database. Attempt to reload
the aviation database. If problem persists, have the G1000 system serviced.
PFD1 DB ERR – PFD1 aviation database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
The MFD and/or PFD detected a failure in the basemap database.
PFD1 DB ERR – PFD1 basemap database error exists.
MFD1 DB ERR – MFD1 terrain dataThe MFD and/or PFD detected a failure in the terrain database. Ensure terrain card
base error exists.
is properly inserted in display. Replace terrain card. If problem persists, have the
PFD1 DB ERR – PFD1 terrain database G1000 system serviced.
error exists.
DB MISMATCH – Aviation database
The PFD and MFD have different aviation database versions installed. Crossﬁll is off.
version mismatch. Xtalk is off.
Install correct aviation database version in both displays.
DB MISMATCH – Aviation database
The PFD and MFD have different aviation database types installed (Americas, European, etc). Crossﬁll is off. Install correct aviation database type in both displays.
type mismatch. Xtalk is off.

GMA 1347 Message Advisories
Alerts Window Message
GMA1 FAIL – GMA1 is inoperative.

Comments
Audio panel self-test has detected a failure. The audio panel is unavailable. Have the
G1000 system serviced.
GMA1 CONFIG – GMA1 conﬁguration Audio panel conﬁguration settings do not match backup conﬁguration memory.
error. Conﬁg service req’d.
Have the G1000 system serviced.
MANIFEST – GMA1 software misThe audio panel has incorrect software installed. Have the G1000 system serviced.
match. Communication halted.
GMA1 SERVICE – GMA1 needs
Audio panel self-test has detected a problem in the unit. Certain audio functions
service. Return unit for repair.
may still be available and the audio panel may still be usable. Have the G1000
system serviced when possible.
BACKUP PATH – Audio panel using
The audio panel is using a backup communication path. Have the G1000 system
backup data path.
serviced when possible.

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Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

GIA 63 Message Advisories
Alerts Window Message
Comments
GIA1 CONFIG – GIA1 conﬁguration
error. Conﬁg service req’d.
GIA1 and/or GIA2 conﬁguration settings do not match backup conﬁguration memory.
Have the G1000 system serviced.
GIA2 CONFIG – GIA2 conﬁguration
error. Conﬁg service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm
up to operating temperature.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over temperature.
GIA1 and/or GIA2 temperature is too high. If problem persists, have the G1000
GIA2 COOLING – GIA2 over tempera- system serviced.
ture.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA1 and/or GIA2 self-test has detected a problem in the unit. Have the G1000
system serviced.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
MANIFEST – GIA1 software mismatch.
Communication halted.
The GIA1 and/or GIA 2 has incorrect software installed. Have the G1000 system
MANIFEST – GIA2 software mismatch. serviced.
Communication halted.
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. Have the G1000 system 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, have the G1000 system 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
have the G1000 system serviced.
transfer key is stuck.
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

105

APPENDIX A

GIA 63 Message Advisories (Cont.)
Alerts Window Message
Comments
RAIM UNAVAIL – RAIM is not availGPS satellite coverage is insufﬁcient to perform Receiver Autonomous Integrity
able from FAF to MAP waypoints.
Monitoring (RAIM) from the FAF to the MAP waypoints.
RAIM UNAVAIL – RAIM is not availGPS satellite coverage is insufﬁcient to perform Receiver Autonomous Integrity
able.
Monitoring (RAIM) for the current phase of ﬂight.
POSN ERROR – RAIM has determined When a RAIM position error is detected, GPS is ﬂagged and the system no longer
GPS position is in error.
provides GPS-based guidance.
DGRD GPS ACC – GPS position acGPS position accuracy has been degraded and RAIM is not available.
curacy degraded & RAIM unavailable.
GPS1 FAIL – GPS1 is inoperative.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is
unavailable. Have the G1000 system serviced.
GPS2 FAIL – GPS2 is inoperative.
GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
GPS2 SERVICE – GPS2 needs service. be available. Have the G1000 system serviced.
Return unit for repair.
NAV1 SERVICE – NAV1 needs service.
Return unit for repair.
A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
NAV2 SERVICE – NAV2 needs service. be available. Have the G1000 system serviced.
Return unit for repair.
NAV1 RMTXFR – NAV1 remote transThe remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”)
fer key is stuck.
state. Press the transfer switch again to cycle its operation. If the problem persists,
NAV2 RMTXFR – NAV2 remote trans- have the G1000 system serviced.
fer key is stuck.

106

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

GIA 63 Message Advisories (Cont.)
Alerts Window Message
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 glideslope receiver 1 and/or receiver 2. Have the
G1000 system serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver
may still be available. Have the G1000 system serviced when possible.

GEA 71 Message Advisories
Alerts Window Message
GEA1 CONFIG – GEA1 conﬁguration
error. Conﬁg service req’d.
MANIFEST – GEA1 software mismatch. Communication halted.
BACKUP PATH – EIS using backup
data path.

Comments
GEA 71 conﬁguration settings do not match those of backup conﬁguration memory.
Have the G1000 system serviced.
The GEA 71 has incorrect software installed. Have the G1000 system serviced.
The GEA 71 is using a backup communication path. Have the G1000 system
serviced when possible.

GTX 33 Message Advisories
Alerts Window Message
Comments
XPDR1 CONFIG – XPDR1 conﬁg error. Transponder conﬁguration settings do not match those of backup conﬁguration
Conﬁg service req’d.
memory. Have the G1000 system serviced.
MANIFEST – GTX1 software misThe transponder has incorrect software installed. Have the G1000 system serviced.
match. Communication halted.
BACKUP PATH – Transponder using
The transponder is using a backup communications path. Have the G1000 system
backup data path.
serviced when possible.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

107

APPENDIX A

GRS 77 Message Advisories
Alerts Window Message
AHRS TAS – AHRS not receiving
airspeed.
AHRS GPS – AHRS using backup GPS
source.
AHRS GPS – AHRS not receiving GPS
information.
MANIFEST – GRS1 software mismatch.
Communication halted.
BACKUP PATH – AHRS using backup
data path.
AHRS SERVICE – AHRS Magnetic-ﬁeld
model needs update.
GEO LIMITS – Too far North/South, no
magnetic compass.

Comments
The AHRS is not receiving true airspeed from the air data computer. The AHRS relies
on GPS information to augment the lack of airspeed. Have the G1000 system
serviced.
The AHRS is using the backup GPS path. Primary GPS path has failed. Have the
G1000 system serviced when possible.
The AHRS is not receiving any GPS information and not operating in its normal mode.
Have the G1000 system serviced.
The AHRS has incorrect software installed. Have the G1000 system serviced.
The AHRS is using a backup communications data path. Have the G1000 system
serviced when possible.
The AHRS earth magnetic ﬁeld model is out of date. Update magnetic ﬁeld model
when practical.
The aircraft is outside geographical limits for approved AHRS operation. Heading is
ﬂagged invalid.

GMU 44 Message Advisories
Alerts Window Message
HDG FAULT – A magnetometer fault
has occurred.
MANIFEST – GMU1 software mismatch. Communication halted.

108

Comments
A fault has occurred in the GMU 44. Heading is ﬂagged invalid. AHRS uses GPS for
backup mode operation. Have the G1000 system serviced.
The GMU 44 has incorrect software installed. Have the G1000 system serviced.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

APPENDIX A

GDC 74A Message Advisories
Alerts Window Message
Comments
GDC1 CONFIG – GDC1 conﬁguration GDC 74A conﬁguration settings do not match those of backup conﬁguration
error. Conﬁg service req’d.
memory. Have the G1000 system serviced.
MANIFEST – GDC1 software misThe GDC 74A has incorrect software installed. Have the G1000 system serviced.
match. Communication halted.
BACKUP PATH – Airdata using backup The GDC 74A is using a backup communications data path. Have the G1000 system
data path.
serviced when possible.

Miscellaneous Message Advisories
Alerts Window 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 that exist in a ﬂight plan that are 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 wayThe system has detected that a waypoint coordinate has changed due to a new
point 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 a 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 approach or arrival used by a stored ﬂight plan. The obsolete procedure is removed
truncated.
from the ﬂight plan. Update ﬂight plan with current arrival or approach.
APPR VPROF – Approaching VNAV
Aircraft is approaching VNAV proﬁle. Prepare to climb or descend to meet VNAV
proﬁle.
proﬁle.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

109

APPENDIX A

Miscellaneous Message Advisories (Cont.)
Alerts Window Message
Comments
APPR TRG ALT – Approaching target
Aircraft is approaching target altitude. Prepare to level aircraft.
altitude.
LOCKED FPL – Cannot navigate locked This occurs when the pilot attempts to activate a stored ﬂight plan that contains
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.
Aircraft is inside airspace.
ARSPC AHEAD – Airspace ahead less
Airspace is ahead of aircraft. Aircraft will penetrate airspace within 10 minutes.
than 10 minutes.
ARSPC NEAR – Airspace near – less
Airspace is within 2 nm of the aircraft position.
than 2 nm.
LEG UNSMOOTH – Flight plan leg will The approaching ﬂight plan waypoints are too close to make smooth turns. Prepare
not be smooth.
for steep turns ahead and expect noticeable course deviations.
APPR INACTV – Approach is not
The system notiﬁes the pilot that the loaded approach is not active. Activate apactive.
proach when required.
SLCT AUTOSEQ – Select auto seThe system notiﬁes the pilot to select auto-sequence mode. Press the OBS softkey to
quence mode.
deactivate the OBS mode.
The system notiﬁes the pilot to load the approach frequency for the appropriate NAV
SLCT FREQ – Select appropriate
frequency for approach.
receiver. Select the correct frequency for the approach.
SLCT NAV – Select NAV on CDI for
The system notiﬁes the pilot to set the CDI to the correct NAV receiver. Set the CDI
approach.
to the correct NAV receiver.
NO WGS84 WPT – Non WGS 84
The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position
waypoint for navigation -[xxxx]
with alternate navigation sources.
TRAFFIC FAIL – Trafﬁc device has
The trafﬁc information system TIS has failed. Have the G1000 system serviced.
failed.
STRMSCP FAIL – Stormscope has
The Stormscope has failed. Have the G1000 system serviced.
failed.

110

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

INDEX
A
Accomplishing a Holding Pattern 94
Activate a Flight Plan 79
Active Flight Plan 71
Active Flight Plan Page 75
Active Flight Plan Page Options 75
AIRCRAFT ALERTS 99
Airspeed Indicator 17
Airspeed Trend Vector 17
Air Data Computer 1
Alerting System 97
Alerts 97
Altimeter 20
Altitude Reference Bug 20
Altitude Trend Vector 20
ALT mode 29
Annunciator lights 34
Approaches 83
Approach markers 38
Inner 38, 43
Lamp color 39
Middle 38
Outer 38, 43
Signal Augmentation 38
ARC HSI 24
ARINC leg types 83
Arrivals and Departures 82
ATC vectors 92
Attitude 1
Attitude Indicator 18
Audio panel controls
ADF 36, 37, 40
AUX 36, 37, 40
COM1 33, 34, 35, 36, 37
COM1 MIC 31, 33
COM2 33, 34, 35, 36, 37
COM2 MIC 31, 33
COM3 33, 35, 36, 37
COM3 MIC 31, 33
COM 1/2 33, 35, 36, 37
COPLT 41
DME 36, 37, 40
NAV1 34, 36, 37, 40

NAV2 34, 36, 37, 40
SPKR 34, 37, 40
SQ 34, 42, 43, 44
TEL 35
VOL 42, 43, 44
Automated Airborne Determination 29
Auto Zoom 54
Aviation Map Data 54

backlighting 12
Backup 44
Barometric Setting Box 20

Fail-safe mode 34
FCC xi
Flight Planning 75
Flight Plan Catalog Page 78
Flight Plan Catalog Page Operations
79
Flight Plan Catalog Page Options 79
Flying the DME ARC 92
Flying the Procedure Turn 90
FMS 1
Fuel Flow indicator 49
Fuel Quantity 47

Caution xi
CDI scaling 85
Change Fields 78
Changing the Map Scale 63
Communications Frequency window
27
COM swap 36
Conﬁguration mode 36, 37, 38, 40
Copyright i
Copy a Flight Plan 80
course deviation indicator 25
Create a New Flight Plan 80

GMA 1347 1
GND mode 29
GPS x

H
Heading Indication 25
Headset(s) 33, 34, 40
Monaural headset 33
Mono 33
Stereo 33
HI SENS 34, 38
Horizontal Situation Indicator 24
hottest cylinder 49

Default power-on settings 34
Delete All Flight Plans 81
Delete a Flight Plan 80
Delete a Waypoint 77
Direct-To Navigation 70
Direct-to Page 70
Direct-to Waypoint 71
DISPLAY BACKUP 34, 44

IDENT 29
INTEG 26
Intercom system (ICS) 41, 43
interrogations 29
Invert and Activate a Flight Plan 80

Jeppesen x

edit a ﬂight plan 77
Engine Indication System 47
ENGINE softkey 45, 47

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111

INDEX
K
Key 3, 4

L
LED 34
Lightning 66
LTNG 58
lying the Missed Approach 88

M
Magnetometer 1
Manual squelch (MAN SQ) 34, 42,
43, 44
Override 43
MAP 58
Map Group Options 60
Map Orientation 54
Map Panning 55
Map Scale 54
Marker beacon 38
Marker Beacon Annunciations 22
MASQ 40
Menus 51
Message Advisories 103, 104, 106,
107, 108, 109, 110
MFD 1, 45
MFD softkeys 45
MKR/MUTE 38
Mode A 29
Mode C 29
Mode S Transponder 29
MUSIC #1 33, 41
MUSIC #2 33, 41

N
NAV1 34, 36, 37, 40
NAV2 34, 36, 37, 40
NAVAID x
NAVAIDS xi
Navigation Frequency window 27
Navigation Map Page 52
112

Navigation Map Page Options Menu
60
navigation source 26
Navigation Status Bar 28
Nearest Airport 72
No Procedure Turn 86

O
OBS 26
Operation 34
Operational x

P
PA 33, 36, 37
Page groups 50
PFD 1, 35, 38, 43
PILOT 41
Pitch Indication 18
PLAY 34
Point-n-Shoot Flight Plan Creation
Feature 81
pounds per square inch 49
Power 63
Power-Up Test 63
Primary Flight Display 9
Procedures 82
Procedures Page 82
PTT 36

R
Range 66
Registered Trademark i
Remove Departure, Arrival, or Approach
77
Reversionary mode 44
Revision ii
revolutions per minute 47
RX 35

S
SD card 4
Selecting Approaches 84

Slip/Skid Indicator 19
Softkey
ENGINE 45
LTNG 58
SYSTEM softkey 45
softkeys 13
Sort By Comment/Number 81
Speaker 37
Special Position Identiﬁcation 29
Specifying a Course to a Waypoint 73
Speed Indication 17
Speed Ranges 17
Spell N Find 71
SPKR 34, 37, 40
Split COM 33, 36
standby mode 29
Stop Navigating a Flight Plan 79
Store Flight Plan 77
SUSP 26
System Annunciations 97
system annunciations 100

T
TCAS symbology 63
TEL 35
Terrain x
Terrain data 66
Terrain Information 57
Terrain Proximity Page 66, 68
Terrain separation x
TIS 57
TIS information 61
TIS Symbology 62
TIS Trafﬁc Advisory 64
TIS Trafﬁc Status 65
Topographic Information 57
Trademark i
Trafﬁc 57, 58
Trafﬁc advisories 61
Trafﬁc Banner 65
Trafﬁc Map Page 61
Trafﬁc Map Page Operations 63
Transponder Status Bar 29

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

INDEX
True Airspeed box 17
Turn Rate Indicator 25
TX 35

V
Vectors to the DME ARC 94
Vertical Deviation/Glideslope Indicator 22
Vertical Speed Indicator 23
Vertical Speed Pointer 23
VFR 29
VLOC receiver 85
Volume 35, 36, 43
Volume/squelch 42
Vspeed References 17

W
WARN 26
Warning 33
Warnings x, xi
Warranty ix

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

113

INDEX

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114

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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.
Unit 5, The Quadrangle
Abbey Park Industrial Estate
Romsey, SO51 9DL, U.K.
p: 44/1794.519944 f: 44/1794.519222
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com

190-00450-00 Rev. B

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