Garmin G1000 cockpit reference guide for Mooney M20M M20R

G1000

cockpit reference guide

for Mooney M20M & M20R

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

COPYRIGHT

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 Printed in the U.S.A.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

RECORD OF REVISIONS

Revision Date of Revision Affected Pages Description

10/19/04

i - xii,

Production Release

1 - 114

11/02/24

i - xii,

Update SW number.

1 - 114

ECO Number

27851

28077

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Record of Revisions ii

Table of Contents iii

List of Figures vi

List of Tables viii

WARRANTY ix

Warnings and Cautions x

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 Speed Ranges Airspeed Trend Vector Vspeed References True Airspeed Box

Attitude Indicator 18

Pitch Indication Roll Indication Slip/Skid Indication

Altimeter 20

Altitude Values Altitude Reference Bug Altitude Trend Vector Altitude Reference Box Barometric Setting Box Altitude Alerting

20 20

Metric Display

Vertical Deviation/Glideslope Indicator 22 Marker Beacon Annunciations 22 Vertical Speed Indicator 23

Vertical Speed Pointer

Horizontal Situation Indicator 24

Heading Indication Turn Rate Indicator Course Deviation Indicator Bearing Pointers and Information Windows Navigation Source

2.4 Communication, Navigation & Surveillance ..... 28

Communication Frequency Window 28 Navigation Frequency Window 28 Navigation Status Bar 29 Transponder Status Bar 30

Transponder Operation Transponder Code Selection

2.5 Alerts and Annunciations ...................................... 30

25 25

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 Intercom Squelch Threshold Control

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

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 Clearing Lightning Data Selecting a Map Range Using the Auto Zoom Feature Identifying Aviation Map Data Decluttering the Map Map Panning

Displaying Topographic Data on the Navigation Map Page

Displaying Terrain Data on the Navigation Map Page Displaying Trafﬁc on the Navigation Map Page

Displaying Lightning Data on the Navigation Map Page Lightning Data Display Range

MFD Navigation Status Window 59 Navigation Map Page Menu 60

First Option: ‘MAP SETUP’ Map Group Orientation

4.5 Trafﬁc Map Page ..................................................... 61

TIS Symbology 63 Trafﬁc Map Page Operations 63

Power-Up Test Changing the Map Range Operating Mode TIS Audio Alert TIS Trafﬁc Status Trafﬁc Banner

4.6 Weather Map Page ................................................. 66

Weather Display Information

Weather Map Page Operations 67

Lightning Strike Symbols

4.7 Terrain Proximity Page .......................................... 68

Terrain Proximity Page Operations 68 Displaying Obstacle Data 69

Obstacle Shapes Navigation Map Display Conditions

4.8 Direct-To Navigation .............................................. 70

Direct to Navigation Operations 71

Selecting a Direct-to Waypoint

Selecting a Direct-to Destination by Facility or City Name

Selecting a Direct-to Destination from the Active Flight Plan

Selecting a Nearest Airport as a Direct-to Destination Shortcuts Canceling Direct-to Navigation Specifying a Course to a Waypoint

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 Create a New Flight Plan Delete a Waypoint

Remove Departure, Arrival, or Approach

Flight Plan Catalog Page 78

Flight Plan Catalog Page Operations Activate a Flight Plan

Stop Navigating a Flight Plan Invert and Activate a Flight Plan Copy a Flight Plan Delete a Flight Plan Delete All Flight Plans

Point-n-Shoot Flight Plan Creation Feature

4.10 Procedures ................................................................ 82

Arrivals and Departures 82 Approaches 83

G1000 Navigational Guidance for Approaches

Selecting Approaches 84 GPS Approach Examples 86

No Procedure Turn

Flying the Missed Approach Flying the Procedure Turn Flying the DME ARC Flying a Holding Pattern

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 111

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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 PFD 39

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

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

LIST OF FIGURES

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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-navi-

gational 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 NAVi

gation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.

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

This page intentionally left blank.

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

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 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 Sys

tem.

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.

• 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 2 4 6

Figure 1-1 G1000 Controls

NAV VOL/ID Control

NAV Frequency Toggle Key

NAV Frequency Selector

Heading Selector

Joystick

Course/Baro Selector

COM Frequency Selector

COM Frequency Toggle Key

COM VOL/SQ Control

Direct-to Key

Flight Plan Key

Clear Key

Flight Management System (FMS) knobs

Menu Key

Procedures Key

Enter Key

Altitude Reference 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 refer- ence 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

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.

MFD Power Up

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 data base 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

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

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 in formation (which is loaded in the system) is displayed (valid operating dates, cycle number and database type indicated).

Press the acknowledge the list information and proceed to the Navi gation Map Page. When the system has acquired a sufﬁcient number of satellites to determine a position, the aircraft symbol appears showing your present position.

ENT key (or the right most softkey) to

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.

1.6 REVERSIONARY MODE

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 selec-

tors, 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.

tomatically 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.

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.

In normal operating mode, the PFD displays graphical

Should a failure occur in either display, the G1000 au

Reversionary display mode can also be manually

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

Figure 1-3 G1000 Normal Mode

SECTION 1 – INTRODUCTION

Figure 1-4 G1000 Reversionary Mode: Failed PFD

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 1 – INTRODUCTION

This page intentionally left blank.

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 con ﬁgured 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 fre quencies 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

Figure 2-1 Default PFD Information

NAV Frequency Window

Airspeed Indicator

True Airspeed Box

Heading Box

Horizontal Situation Indicator

Outside Air Temperature Box

System Time Box

Transponder Status Bar

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Turn Rate Indicator

Barometric Setting Box

Vertical Speed Indicator

Altimeter

Altitude Reference Box

COM Frequency Window

Navigation Status Bar

Slip/Skid Indicator

Attitude Indicator

SECTION 2 – PFD

Figure 2-2 Additional PFD Information

Trafﬁc Annunciation

Selected Heading Box

Inset Map

BRG1 Information Window

BRG2 Information Window

Alerts Window

Selected Course Box

Annunciation Window

Vertical Deviation/Glideslope Indicator

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 inten sity 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 back-

lighting 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:

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

1. Press the

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

2. Turn the Turn the

large FMS small FMS

knob to highlight PFD DSPL.

knob in the direction of the

green arrow to display PFD KEY.

3. Turn the Turn the

large FMS

small FMS

tion window. Turn the ‘MANUAL’, then press the

knob to highlight ‘AUTO’. knob to display the selec-

FMS

knob to select

ENT

key.

4. With the intensity value now highlighted, turn the

small FMS

backlighting, then press the

5. Turn the

large FMS

and turn the

knob to select the desired

ENT

key.

knob to highlight MFD DSPL

small FMS

knob in the direction of

the green arrow to display MFD KEY. Repeat

CLR

steps 3 and 4. Press the

key to

remove the window.

1. Press the

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

2. Turn the

small FMS

tion window. Turn the ‘MANUAL’, then press the

knob to display the selec-

FMS

knob to select

ENT

key.

3. With the intensity value now highlighted, turn the

small FMS

backlighting, then press the Turn the large FMS knob to highlight ‘AUTO’ next

knob to select the desired

ENT

key.

to ‘MFD DSPL’ and repeat steps 2 and 3. Press the

CLR

key to remove the window.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Figure 2-3 PFD Setup Menu

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 ALERTS softkeys change momentarily to black text on gray background and automatically switches back to white text on black background.

Softkey On

The PFD softkeys listed provide control over ﬂight management functions including GPS, NAV, terrain, traf ﬁc and lightning.

INSET – Press to display the Inset Map in the lower

left corner of the PFD.

OFF DCLTR

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

map.

TOPO

coastlines, terrain, rivers, lakes, etc.) and elevation scale on the inset map.

TERRAIN

on the inset map.

LTNG

the inset map (within a 200 nm radius of the aircraft).

BACK

softkey conﬁguration.

CDI, IDENT, TMR/REF, NRST and

Softkey Off

– Press to remove the Inset Map

(3) – Press momentarily to select the

– Press to display TIS trafﬁc on the

– Press to display topographical data (i.e.,

– Press to display terrain information

– Press to display the lightning data on

– Press to return to the previous level

PFD – Press to display the additional softkeys for

additional conﬁgurations to the PFD.

METRIC

DFLTS BRG1

360 HSI ARC HSI BRG2

STD BARO

BACK

– 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.

– Press to reset default settings on the PFD.

– Press to display the BRG (bearing) 1 infor-

mation 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.

– Press to display the 360° compass rose.

– Press to display the 140° viewable arcs.

– Press to display the BRG (bearing) 2 infor-

mation 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.

– Press to set the barometric pressure to 29.92 inches of mercury (1013 hPa by pressing the METRIC softkey).

– Press to return to the previous level softkeys.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SECTION 2 – PFD

INSET

OFF

TOPO

TRAFFIC

TERRAIN

DCLTR

DCLTR-2

DCLTR-3

DCLTR-1

BACK

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

ALERTS

PFD

METRIC

DFLTS

ARC HSI

360 HSI

STD BARO

BACK

Press the BACK softkey to return to the top level softkeys

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

ALERTS

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Figure 2-4 PFD Softkeys (1 of 2)

SECTION 2 – PFD

NRST

OBS

CDI

TMR/REF

IDENT

ALERTS

XPDR

STBY

BACK

VFR

ALT

CODE

IDENT

BACK

BKSP

Press the BACK softkey to return to the top level softkeys

ALERTS

CDI (NAV1)

CDI (NAV2)

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 selec-

tion softkeys.

STBY

– Press to select standby mode.

– 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 IDENT

– Press numbers to enter code.

– 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

+ 100 hidden pages