Garmin G1000 cockpit reference guide for Mooney M20M M20R

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G1000

cockpit reference guide

for Mooney M20M & M20R

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Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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.

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WARNINGS & CAUTIONS

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Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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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

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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

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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.

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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

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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

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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

Page 21

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

Page 22

SECTION 1 – INTRODUCTION

This page intentionally left blank.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 23

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

Page 24

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

Page 25

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

Page 26

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

Page 27

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

Page 28

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)

Page 29

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

Page 30

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

Page 31

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 infor mation is also displayed:

• Speed indication

• Speed ranges

• Airspeed trend vector

• Vspeed references

Airspeed Trend

Vector

Actual Airspeed

True Airspeed

Box

Figure 2-5 Airspeed Indicator

Vspeed

References

Speed Ranges

Speed Indication

The numeric labels and major tick marks on the mov ing 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 air speed is displayed inside the black pointer. The pointer remains black until reaching never exceed speed (Vne), at which point it turns red.

Speed Ranges

A color coded (white, green, yellow, and red) speed range strip is located on the moving tape. The colors de note ﬂaps operating range, normal operating range, cau

tion 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.

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 air speed will be in 6 seconds if the current rate of accelera

tion is maintained. The trend vector is absent if the speed remains constant and if any data needed to calculate air

speed 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

Page 32

SECTION 2 – PFD

Attitude Indicator

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

Pitch Indication

Major pitch marks and numeric labels at 10, 20, 30,

40, 50, 60, 70 and 80 degrees are shown above and be

low 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).

Roll Pointer

Roll Scale

Horizon Line

Aircraft Symbol

Land Representation

Aircraft Wing Tips

Pitch Scale

Figure 2-7 Attitude Indicator

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Slip/Skid Indicator

Sky Representation

Roll Index

Page 33

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 indi

cates 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

Figure 2-9 Attitude Indicator Nose Low

Slip/Skid Indication

The Slip/Skid indicator resides beneath the roll pointer. The indicator moves with the roll pointer and moves later ally 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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 34

SECTION 2 – PFD

Altimeter

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

• 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

Current Altitude

Altitude Reference Bug

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

The vertical, magenta line extends up or down the alti

tude 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 alti

tude in feet. The metric value, when selected, is displayed on top the Altitude Reference box.

Barometric Setting Box

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

Barometric Setting

Box

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

To select barometric pressure:

1. Turn the large BARO (outer) knob to select

the desired setting.

Page 35

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 func

tion 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 ref

erence 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 pass

es through +/- 1,000 ft. of the reference altitude.

When the aircraft passes within +/- 200 ft. of the ref

erence altitude, the reference altitude ﬂashes (cyan on black) again indicating that the aircraft is within the devia

tion 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.

SECTION 2 – PFD

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

Figure 2-11 Colors Associated with the Altitude Alerter

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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

Page 36

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. Press the

PFD softkey to display the second

level softkeys.

2. Press the METRIC softkey to display altitude in

meters and barometric pressure in hectopascals.

BACK

Press the

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

Figure 2-14 Altimeter (Metric)

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Vertical

Deviation/Glideslope

Indicator

Figure 2-16 Marker Beacon and Vertical Deviation

Page 37

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.

SECTION 2 – PFD

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

Page 38

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

Lateral Deviation

Scale

Course Deviation and

TO/FROM Indicator

Figure 2-17 ARC HSI

Figure 2-18 Horizontal Situation Indicator

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

Page 39

SECTION 2 – PFD

Heading Indication

A digital reading of the current magnetic heading ap

pears 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

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.

Course Deviation Indicator

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 dis

played 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.

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

Page 40

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 point

ers 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 2

Pointer

Bearing 1

Information

Window

Figure 2-22 HSI with Bearing Information

Distance from

Waypoint

Waypoint Identiﬁer

Bearing

Source

Figure 2-23 BRG1 Information Window

Pointer

Icon

Figure 2-24 BRG2 Information Window

Bearing 1

Pointer

Bearing 2

Information

Window

Pointer

Icon

Distance from

Waypoint

Identiﬁer

Bearing

Source

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 41

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 auto

matic sequencing of waypoints. OBS mode also allows the pilot to set the desired course TO/FROM a waypoint.

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.

2. Press the

CDI softkey again to change from

NAV1 to NAV2. This will place the cyan tuning box over the NAV2 standby frequency.

To enable/disable OBS mode while navigating with GPS

1. Press the

OBS softkey to select OBS Mode.

2. Turn the small CRS knob to select the desired

course TO/FROM the waypoint.

3. Press the OBS softkey again to return to normal

operation.

3. Press the GPS.

CDI

softkey a third time to return to

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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

Page 42

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 Communica-

tion Frequency window are located in the VHF NAV/COM Pilot’s Guide.

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.

Selected COM

Frequency

(Green)

Figure 2-26 Communication Frequency Window

NAV Receivers

Active COM

Frequency Field

Frequency

Toggle Arrow

Frequency

Tuning Box

Standby NAV

Frequency Field

Figure 2-27 Navigation Frequency Window

Frequency

Tuning Box

Standby COM

Frequency Field

Active NAV

Frequency Field

Frequency

Toggle Arrow

COM Radios

Selected NAV

Frequency

(Green)

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Page 43

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.

Distance to

Next Waypoint

Desired Track

Next Waypoint

SECTION 2 – PFD

Current Track

Figure 2-28 Navigation Status Bars

Figure 2-29 Navigation Status Bar Message

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Page 44

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 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 land ing 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 tran- sponder 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 exter nal altitude source, which is not adjusted for baro metric 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-pro-

Automated

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 se

quence. 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.

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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 cen ter, 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 con trols 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: Refe r to the Audio Pane l Pilo t’s

Guide Supplement for Mooney for addit i on a l i n f or m at i on r eg a r d i n g t h e 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)

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SECTION 3 – AUDIO PANEL

Transmitters

Split COM

Passenger Address

Marker Beacon/Mute

Aircraft Navigation Radio Audio

Manual Squelch

Transceiver Audio

Telephone

Speaker

Marker Beacon Signal Sensitivity

Aircraft Navigation Radio Audio

Digital Recording Playback

ICS Isolation

VOL/SQ

VOL Annunciation

Figure 3-1 Front Panel Controls

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

SQ Annunciation

Reversionary Mode

Page 47

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.

Mono/Stereo Headsets

The GMA 1347 can accommodate up to six (6) headsets (pilot, copilot and up to four (4) passengers).

In Conﬁguration mode, headset audio level can be ad

justed 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

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.

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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 approxi mately 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 de-

activates 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 opera-

tions, its corresponding annunciator LED is lit.

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SECTION 3 – AUDIO PANEL

Transceiver Keys

As illustrated below, the following eight (8) transceiv-

er 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.

NOTE: A PTT switch must be pressed to allow

all microphone transmissions.

Pressing a COM 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.

During COM signal reception, a white RX inscrip

tion 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 al ready 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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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 MASQ

is present-

ed 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).

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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 ef fect 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

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.

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.

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.

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SECTION 3 – AUDIO PANEL

Split COM and PA

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.

NOTE: Only the copilot can make PA announce-

ments when in split COM and PA mode.

Speaker Output

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.

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

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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 indica tor 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.

When the

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

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 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.

The lamp and audio keying of the marker beacon re ceiver 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.

NOTE: The marker beacon receiver lights operate

independently of the marker beacon audio and cannot be turned off.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Figure 3-4 Marker Beacon

NOTE: The marker beacon signal sensitivity

threshold can be set in Conﬁguration mode. Please consult a Garmin-authorized service center for details.

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SECTION 3 – AUDIO PANEL

Beacon Audio Frequency Audio Keying Rate Lamp Color

Outer Marker

Middle Marker

Airway/Inner Marker

Inner Marker Middle Marker Outer Marker

400 Hz — — — 2 dashes per second Blue

1,300 Hz • — • —

95 dot-dash combinations

per minute

Amber

3,000 Hz • • • • 6 dots per second White

Table 3-1 Marker Beacon Signal Characteristics

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

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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.

If desired, the disabled. Please consult a Garmin-authorized service center for details.

DME, ADF and AUX channels may be

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.

Figure 3-6 Aircraft Radios

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Page 55

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.

SECTION 3 – AUDIO PANEL

Figure 3-7 ICS Isolation

PILOT 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.

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 COPILOT CREW ALL

PILOT Key Press

COPLT Key Press

ALL CREW COPILOT PILOT

CREW ALL PILOT COPILOT

Table 3-2 ICS Isolation Mode Transitions

CREW Mode

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 and

can also communicate with each other, while the pas-

sengers can only hear MUSIC 2.

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

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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 Hears Copilot Hears Passenger Hears

PILOT

Selected radios; pilot Copilot; passengers; MUSIC 1 Copilot; passengers; MUSIC 1

(PILOT LED Lit)

COPILOT

(COPLT LED Lit)

CREW

(Both LEDs Lit)

(Both LEDs OFF)

ALL

Selected radios; pilot; passengers; MUSIC 1

Selected radios; pilot; copilot; MUSIC 1

Selected radios; pilot; copilot; passengers; MUSIC 1

Table 3-3 ICS Operation Modes

3.6 VOLUME/SQUELCH CONTROL

Copilot; MUSIC 2 Selected radios; pilot;

passengers; MUSIC 1

Selected radios; pilot; copilot;

Passengers; MUSIC 2

MUSIC 1 Selected radios; pilot; copilot;

passengers; MUSIC 1

Selected radios; pilot; copilot; passengers; MUSIC 1

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.

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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 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 at the lower right of the press the

VOL/SQ

knob to toggle to ICS volume

VOL/SQ

adjustment mode, and turn the appropriate

VOL/SQ

knob.

VOL/SQ

annunciation

knob is lit),

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 per

formed 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 adjust-

ments, 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

1. Press the

key is not annunciated: MAN SQ

key and perform one of the

following steps:

VOL

2a. If the

annunciation is lit, press the knob to illuminate the turn the

2b. If the

VOL/SQ

annunciation is already lit, turn the

knob.

annunciation, and

VOL/SQ

1b. If the unit is already in ICS volume adjustment

VOL

mode (i.e., if the lower left of the appropriate

VOL/SQ

annunciation at the

VOL/SQ

knob is lit), turn the

knob.

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SECTION 3 – AUDIO PANEL

To adjust squelch threshold level manually if the

MAN SQ

1a. If the

key is already annunciated:

VOL

annunciation is lit, press the knob to illuminate the SQ annunciation, and turn the

1b. If the

VOL/SQ

knob.

annunciation is already lit, turn the

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.

VOL/SQ

Figure 3-8 Reversionary Mode

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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.

4.2 MFD SOFTKEYS

The MFD softkeys are located below the display glass and provide control over ﬂight management func tions 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.

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..

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 follow-

ing 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.

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SECTION 4 – MFD

BACK

RST USED

SYSTEM

ENGINE

LEAN

ENGINE

MAP

DCLTR

BACK

SYSTEM

LEAN

ENGINE

LEAN

BACK

SYSTEM

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

TRAFFIC

TOPO

BACK

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

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

CHKLIST

ASSIST

CYL SLCT

LTNG

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

Figure 4-2 MFD Softkeys

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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:

• Engine (default)

• Lean

• System

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 in dicating 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.

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.

Fuel Qty Indicator

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 dis-

play 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.

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SECTION 4 – MFD

Manifold

Pressure

Gauge

Fuel Quantity

Indicator

Oil Pressure

Indicator

Exhaust Gas Temperature

Cylinder Head

Temperature

Indicator

Tachometer

Fuel Flow

Indicator

Oil Temperature

Flaps Position

Indicator

Turbine Inlet Temperature

Indicator

Voltmeter

Ammeter

Rudder Trim

Indicator

Figure 4-3 ENGINE Page (Normally Aspirated)

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Elevator Trim

Indicator

Figure 4-4 ENGINE Page (Turbocharged)

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SECTION 4 – MFD

Fuel Flow Indicator (Normally Aspirated)

The Fuel Flow indicator displays current fuel ﬂow val-

ues, expressed in gallons per hour (GPH).

Fuel Pressure Indicator (Turbocharged Only)

The Fuel Pressure indicator displays current fuel sys-

tem 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 de grees 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

CHT Indicator

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

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.

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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

Figure 4-5 Page Group Window

Currently

selected page is

highlighted

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

Figure 4-6 Page Title Window

Active Page Title

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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.

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 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.

CLR to immediately display the

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.

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.

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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.

2. 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

FMS

knobs, the Navigation Map Page can be

selected from any page by pressing and holding the

CLR

(DFLT MAP) key

large

and

small

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

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Figure 4-8 Navigation Map Page

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SECTION 4 – MFD

Changing the Map Orientation

See the Navigation Map Page Menu section for instruc

tions on how to change the map orientation.

Clearing Lightning Data

See the Navigation Map Page Menu section for instruc

tions on how to clear lightning data from the map dis

play

NOTE: A complete list of available map datums are given in Appendix D of the Pilot’s Guide.

Selecting a Map Range

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.

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.

Map

Range

Figure 4-9 Navigation Map Range

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SECTION 4 – MFD

Decluttering 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.

NOTE: Some of the map features are automati-

cally 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 func

tion 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.

To pan the map:

1. Push in the

joystick

to display the panning

arrow.

2. 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.

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

joystick

NOTE: The airspace boundary stays highlighted

for approximately four seconds before returning to normal shading.

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SECTION 4 – MFD

Distance, bearing

and elevation

Panning

Arrow

Latitude and

longitude

position of

pointer

Figure 4-10 Navigation Map Panning

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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:

MAP

1. Press the

2. Press the

softkey.

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 Naviga

tion 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:

MAP

1. Press the

2. Press the

softkey.

TERRAIN

softkey. Press the

TERRAIN

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

SECTION 4 – MFD

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 Informa-

tion 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:

MAP

1. Press the

2. Press the

TRAFFIC

softkey.

TRAFFIC

softkey. Press the

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.

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SECTION 4 – MFD

To display trafﬁc on the Navigation Map Page:

MAP

1. Press the

2. Press the

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.

softkey.

TRAFFIC

softkey. Press the

softkey again to remove trafﬁc.

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:

softkey.

1. Press the

2. Press the

MAP

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

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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.

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)

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.

• Vertical speed required (VSR)

• Cross track error (XTK)

• Currently selected MFD page title

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.

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)

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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

key to display the Navigation Map Page Menu. The cursor ﬂashes on ‘Map Setup’.

ENT

2. Press the

key. The Map Setup Menu is

displayed.

3. Turn the group and press the

4. Turn the

small FMS

large FMS

knob to select the ‘

ENT

key.

Map’

knob to highlight the

‘ORIENTATION’ ﬁeld.

5. Turn the

small FMS

orientation and press the

6. Press the

FMS

knob to select the desired

ENT

key.

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 head

ing (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.

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4.5 TRAFFIC MAP PAGE

The Trafﬁc Map Page displays the following informa-

tion:

• Current aircraft location, surrounding Trafﬁc Information System (TIS) trafﬁc, and range mark ing 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

FMS

knob to select the Trafﬁc Map Page.

small

SECTION 4 – MFD

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 require ments are not considered evasive maneuvers. See Appendix E in the Pilot’s guide for detailed TIS information.

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SECTION 4 – MFD

Trafﬁc Mode

Trafﬁc

Map Range

Vehicle (ownship)

Figure 4-15 Trafﬁc Map Page

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SECTION 4 – MFD

TIS Symbology

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 Symbol

Trafﬁc

Trafﬁc Map Page Operations

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. Con tact 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.

NOTE: Trafﬁc Information Service (TIS) is not

available in all areas.

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 sys

tem 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.

3. Press the

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 au

dio 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:

MODE

1. Press the

2. Press the

softkey.

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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 80

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.

Display Mode

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.

Current Strike Rate

Range

Marking Rings

Figure 4-16 Weather Map Page

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 81

NOTE: The WX-500 has to be receiving valid

heading information in order for lightning data to be displayed.

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.

SECTION 4 – MFD

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

1. Select the Weather Map Page.

VIEW

2. Press the

softkey. The

keys are displayed. Press the

360

and

ARC

360 softkey to

soft-

display a 360˚ viewing are or press the ARC softkey to display a 120˚ viewing area OR:

3. Press the

key. The page menu is displayed with ‘View Arc’ or ‘View 360’ highlighted. Press the

ENT

key on the desired

selection.

To clear display lightning data from the display:

CLEAR

1. Press the data from the display OR: Press the Select ‘Clear Lightning Data’. Press the

softkey to remove all lightning

key.

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

2. Press the

softkey. The

CELL

MODE

softkeys are displayed. Press the to display ‘CELL’ data or press the 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:

3. Press the

key. The page menu is displayed with ‘Strike Mode’ or ‘Cell Mode’ highlighted. Press the

ENT

key on the desired

selection.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

and

CELL

STRIKE

softkey

STRIKE

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 Symbol

Lightning Strike - Age is 0 - 6 Seconds

Lightning Strike - Age is 6 - 20 Seconds

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

Page 82

SECTION 4 – MFD

1000' AGL

Aircraft Altitude

100' Threshold

4.7 TERRAIN PROXIMITY PAGE

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.

Terrain Proximity Page Operations

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

VIEW

2. Press the

softkey. Press the

key.

3. To return to the 360 degree viewing display

press the 360 softkey OR:

4. 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 the

joystick

clockwise zoom out or turn

counter-clockwise zoom in. Map ranges are 25 nm, 25/50 nm, 50/100 nm, and 100/200 nm.

ARC

soft-

Figure 4-17 Terrain Scale

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 83

SECTION 4 – MFD

Displaying Obstacle Data

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

‘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:

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

Indication

TERRAIN FEATURE

OFF OFF NO OBSTACLES DISPLAYED

OFF ON SAFE, CAUTION, AND WARNING OBSTACLES

ON OFF CAUTION AND WARNING OBSTACLES

ON ON SAFE, CAUTION, AND WARNING OBSTACLES

Color

RED

WARNING: Obstacle height is at or above 100’ below the current aircraft altitude.

CAUTION: Obstacle height is between

YELLOW

100’ and 1000’ below the current aircraft altitude.

GRAY

SAFE: Obstacle height is lower than 1000’ below the current aircraft altitude.

Navigation Map Display Conditions

The Map Setup Page Menu has ‘OBSTACLE’ and

OBSTACLE FEATURE

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.

TERRAIN PROXIMITY PAGE

DISPLAYED

Obstacle Shapes

Unlighted Obstacle (Height is less than 1000’ AGL)

Lighted Obstacle (Height is less than 1000’ AGL)

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Unlighted Obstacle (Height is greater than 1000’ AGL)

Lighted Obstacle (Height is greater than 1000’ AGL)

Page 84

SECTION 4 – MFD

4.8 DIRECT-TO NAVIGATION

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

Flight Plan Way

point Selection

Symbol

Nearest Airport

Selection

Map Orientation

To select a direct-to destination:

1. Press the

Direct-to

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

2. 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.

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

ENT

4. Press the

key to conﬁrm the identiﬁer. The

‘Activate?’ ﬁeld is highlighted.

ENT

5. Press the

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.

Map of the

Selected

Waypoint

Bearing

Distance

Direct-to

Course

Figure 4-18 Direct-to Page

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Map Range

Region

Latitude/

Longitude

Activate Field

To re-center the CDI (HSI) needle to the same destination waypoint:

1. Press the Direct-to key, followed by press ENT

ing the

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.

Page 85

SECTION 4 – MFD

Direct to Navigation Operations

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 fol lowing 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

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:

4. Continue turning the

small FMS

knob to scroll through any additional database listings for the selected facility name or city. The

FMS

knob can be used to scroll backwards if

the desired waypoint was passed up.

ENT

5. Press the point, and

key to conﬁrm the selected way-

ENT

again to activate a Direct-to.

Selecting a Direct-to Destination from the Active Flight Plan

Any waypoint contained in the ﬂight plan may be se lected as a direct-to destination from the Direct-to Way point Page when navigating an active ﬂight plan.

small

1. Press the

Direct-to

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

2. Turn the

large FMS

knob to highlight the facility

or city name ﬁeld.

3. 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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Figure 4-19 Flight Plan Waypoint Direct-to

Page 86

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.

2. Turn the

large FMS

knob to highlight the ﬂight plan ‘FPL’ ﬁeld.

3. Turn the

small FMS

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

4. Continue turning the

small FMS

knob to scroll through the list and highlight the desired waypoint.

ENT

5. Press the point, and

key to conﬁrm the selected way-

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:

1. Press the

Direct-to

key. The Direct-to Page appears with the destination field high lighted.

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 way-

points:

• 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.

2. Turn the

large FMS

knob to highlight the near-

est airport ﬁeld.

3. 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.

ENT

4. Press the point, and

key to conﬁrm the selected way-

ENT

again to activate direct-to.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 87

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:

Figure 4-20 Nearest Airport Direct-to

1. Press the

Direct-to

key to display the Direct-to

Page.

2. Press the

key to display the direct-to

options menu.

3. With Cancel Direct-To NAV highlighted, press the

ENT

key. If a ﬂight plan is still active, the G1000 resumes navigating the ﬂight plan along the closest leg.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 88

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:

1. Press the

2. Turn the

Direct-to

small

key.

and

large FMS

the destination waypoint.

ENT

3. Press the point, then turn the

key to conﬁrm the selected way-

large FMS

knob to highlight

the course ﬁeld.

small

and

4. Turn the

large FMS

the desired course and press the

ENT

5. Press the

key again to begin navigation

using the selected destination and course.

knobs to select

ENT

key.

Figure 4-21 Manual Course Direct-to

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 89

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 way point 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.

to display the following:

Page:

The data ﬁelds are user-selectable and can be changed

• 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

• 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:

FPL

1. Press the to display the Flight Plan Catalog Page.

2. Press the Catalog Page options.

3. Turn the New Flight Plan’ and press the

4. A blank ﬂight plan page appears for the ﬁrst

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

key and turn the

key to display the Flight Plan

large FMS

knob to highlight ‘Create

small FMS

ENT

key.

knob

Page 90

SECTION 4 – MFD

empty storage location. Turn the small and

large FMS

departure waypoint and press the

knobs to enter the identiﬁer of the

ENT

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

6. Once all waypoints have been entered, press

FMS

the

knob to return to the Flight Plan

Catalog Page.

key.

Figure 4-22 New Flight Plan

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 91

SECTION 4 – MFD

To edit a ﬂight plan:

1. Press the

key and turn the

small FMS

knob

FPL

to display the Flight Plan Catalog Page.

2. Press the

3. Turn the

FMS knob

large FMS

desired ﬂight plan and press the

to activate the cursor.

knob to highlight the

ENT

key.

4. 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.

5. To delete a waypoint from the ﬂight plan: Turn

large FMS

the to delete and press the

knob to select the waypoint

CLR

key to display a

remove waypoint conﬁrmation window. With

ENT

‘OK’ highlighted, press the

key to remove

the waypoint. To cancel, turn the large FMS knob to highlight ‘CANCEL’ and press the ENT key.

Delete a Waypoint

To delete a waypoint from an existing ﬂight plan:

1. Press the

key and turn the

small FMS

knob

FPL

to display the Flight Plan Catalog Page.

FMS

2. Press the

3. Turn the desired ﬂight plan and press the

4. Turn the to delete and press the

knob to activate the cursor.

large FMS

knob to highlight the

knob to select the waypoint

CLR

ENT

key.

key to display a

‘REMOVE WAYPOINT’ conﬁrmation window.

ENT

5. With ‘OK’ highlighted, press the

key to remove the waypoint. To cancel the delete request, turn the

large FMS

‘CANCEL’ and press the

knob to highlight

ENT

key.

6. Once all changes have been made, press the

FMS

knob to return to the Flight Plan Page.

6. Once all changes have been made, press the

FMS knob

to return to the Flight Plan Catalog

Page.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

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.

Page 92

SECTION 4 – MFD

To remove an approach, arrival or departure from the active ﬂight plan:

1. From the Active Flight Plan Page, press the

key to display the Active Flight Plan Page

options.

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

ENT

key.

3. A conﬁrmation window is displayed listing the procedure the pilot is about to remove. With

ENT

‘OK’ highlighted, press the the remove request, turn the to highlight ‘CANCEL’ and press the

key. To cancel

large FMS

ENT

knob

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 depar ture, destination, total distance, and enroute safe altitude information.

To display the Flight Plan Catalog Page:

1. Press the

key and turn the

small FMS

FPL

to display the Flight Plan Catalog Page.

Flight Plans

in Memory

knob

Flight Plan List

Figure 4-24 Removing an Approach

Flight Plan

Information

Figure 4-25 Flight Plan Catalog Page

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 93

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

key to

display the Flight Plan Catalog Page options.

4. Turn the

large FMS

Flight Plan’ and press the

knob to highlight ‘Activate

ENT

key.

5. An ‘Activate stored ﬂight plan?’ conﬁrmation window is displayed. With OK highlighted,

ENT

press the cancel the ﬂight plan activation, turn the

FMS

knob to highlight ‘CANCEL’ and press the

ENT

key.

Figure 4-27 Activate Stored Flight Plan Conﬁrmation

key to activate the ﬂight plan. To

large

Stop Navigating a Flight Plan

To stop navigating a ﬂight plan:

1. Press the

key and turn the

small FMS

knob

FPL

to display the Flight Plan Catalog Page.

Figure 4-26 Flight Plan Catalog Page Options

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

key and turn the

small FMS

knob

FPL

to display the Flight Plan Catalog Page.

2. Press the

3. Turn the

FMS knob

large FMS

to activate the cursor.

knob to highlight the

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

FMS

2. Press the

3. Turn the desired ﬂight plan and press the

knob to activate the cursor.

large FMS

knob to highlight the

display the Flight Plan Catalog Page options.

small

4. Turn either the

large FMS

highlight ‘Delete Flight Plan’ and press the 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

to highlight ‘CANCEL’ and press the

key to

knob to

ENT

knob

ENT

key.

Page 94

SECTION 4 – MFD

To copy a ﬂight plan to another ﬂight plan catalog location:

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

key and turn the

small FMS

knob

FPL

to display the Flight Plan Catalog Page.

FMS

2. Press the

3. Turn the desired ﬂight plan and press the

knob to activate the cursor.

large FMS

knob to highlight the

key to

display the Flight Plan Catalog Page options.

4. Turn either the

large FMS

knob to

small

highlight ‘Invert & Activate FPL’ and press the

ENT

key.

5. An ‘Invert and activate stored ﬂight plan?’ confirmation window is displayed. With

ENT

‘OK’ highlighted, press the

key to inverts and activate the ﬂight plan. To cancel the operation, turn the

large FMS

‘CANCEL’ and press the

knob to highlight

ENT

key.

Copy a Flight Plan

‘Copy Flight Plan’ copies the active ﬂight plan to a

Flight Plan Catalog location. The copy function is use

ful for duplicating the active ﬂight plan before making changes.

1. From the Flight Plan Catalog press the knob to activate the cursor, turn the

FMS

knob to highlight the ﬂight plan the pilot

wishes to copy, then press the

FMS

large

key to

display the Flight Plan Catalog Options.

2. Turn the

large FMS

Flight Plan’ and press the

knob to highlight ‘Copy

ENT

key.

3. 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

press the

knob to highlight ‘CANCEL’ and

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

key to display the Active Flight Plan

options window.

2. Turn the

large FMS

Flight Plan’ and press the

3. A ‘Delete all waypoints in ﬂight plan?’ conﬁr

knob to highlight ‘Delete

ENT

key.

mation window is displayed. With ‘OK’ highlighted, press the ﬂight plan. To cancel, turn the to highlight ‘CANCEL’ and press the

ENT

key to delete the active

large FMS

ENT

knob

key.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 95

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.

2. Press the

key to display the Flight Plan

Catalog options.

3. Turn the

large FMS

Flight Plan’ and press the

knob to highlight ‘Delete

ENT

key.

4. A ‘Delete ﬂight plan?’ conﬁrmation window is displayed. With ‘OK’ highlighted, press the

ENT

key to delete the ﬂight plan. To cancel,

turn the and press the

large FMS

ENT

knob to highlight ‘CANCEL’ key.

Delete All Flight Plans

‘Delete All’ removes all ﬂight plans from memory at

one time.

To delete all ﬂight plans:

1. From the Flight Plan Catalog Page, press the

key to display the Flight Plan Catalog

Page options.

2. Turn the All’ and press the

large FMS

knob to highlight ‘Delete

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

FMS

knob to highlight ‘CANCEL’ and press the

ENT

key.

large

Point-n-Shoot Flight Plan Creation Feature

The “Point-n-Shoot” ﬂight plan creation feature is acti

vated using the Navigation Map Page and the Active Flight Plan Page.

1. Push the

Joystick

to turn the map cursor on.

2. Select the Active Flight Plan Page and press

FMS

the Waypoints will be inserted ABOVE the high

knob to highlight the list of waypoints.

lighted row if the cursor is on. Waypoints will be inserted at the END of the ﬂight plan if the cursor is off.

3. To insert waypoints, use the map cursor to point at the desired waypoint (it will become visually enhanced when it is properly pointed

LD WPT

to), and press the

softkey. Existing user

waypoints are inserted in the same manner.

4. 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.

5. 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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 96

SECTION 4 – MFD

4.10 PROCEDURES

Arrivals and Departures

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

To select a departure:

1. Press the

key. Turn the

large FMS

knob

PROC

to highlight ‘Select Departure’ and press the

ENT

key. The departure procedure window

appears.

2. Turn the ture and press the

FMS

knob to select the desired depar-

ENT

key. The transition

window appears.

FMS

3. Turn the

knob to select the desired

transition and press the ENT key. ‘LOAD?’ is

ENT

highlighted. Press the

NOTE: Vector departures are not part of the aviation database.

key.

To select an arrival:

PROC

1. Press the

key. Turn the large

to highlight ‘Select Arrival’ and press the

FMS

knob

ENT

key. The arrival procedure window appears.

FMS

2. Turn the and press the

knob to enter the desired arrival

ENT

key. The transition window

appears.

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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

NOTE: The approach vectors option assumes the pilot will receive vectors to the ﬁnal course segment of the approach and will provide navi gation guidance on the ﬁnal approach segment and extension only.

3. Turn the transition and press the highlighted. Press the

FMS

knob to select the desired

ENT

key. ‘LOAD?’ is

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.

Page 97

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 guid ance 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 guid-

ance 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

Page 98

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:

PROC

1. Press the Page. Turn the ‘Select Approach’ and press the approach procedure window appears.

2. Turn the approach and press the window appears.

key to display the Procedures

large FMS

knob to highlight

ENT

FMS

knob to select the desired

ENT

key. The transition

key. The

Figure 4-30 Selecting an Approach Procedure

3. Turn the tion and press the highlighted. Press the

FMS

knob to select the desired transi-

ENT

key. ‘LOAD?’ is now

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. ‘Acti vate?’ 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.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Figure 4-31 Selecting an Approach Transition

Page 99

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. Acti

vating 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

PROC

plan, press the

key to display the Proce-

dures Page.

2. Turn the

large FMS

knob to highlight ‘Activate

Approach’.

ENT

3. Press the

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

key.

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 100

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

FPL

approach without pilot input other than to activate the ap proach 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. Select KPRC as the destination, via the

Direct-to

key or as the last waypoint in a ﬂight plan.

2. Press the

PROC

key and select the GPS RWY 12 approach. From the transitions window, select IRODY as the IAF (select ‘LOAD?’).

3. 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.

4. Prior to reaching the IAF (IRODY), the approach sequence should be reviewed. Press the 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

FPL

ﬁnished press the

key again to return to

the previous page.

5. 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°’.

6. 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°’.

7. 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.

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

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

10. Upon crossing the MAP, ‘SUSP’ appears on the

SUSP

HSI and directly above the

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 avail-

able’ 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

Garmin G1000 cockpit reference guide for Mooney M20M M20R

Specifications and Main Features

Frequently Asked Questions

User Manual

COPYRIGHT

RECORD OF REVISIONS

TABLE OF CONTENTS

LIST OF FIGURES

LIST OF TABLES

WARRANTY

SECTION 1: INTRODUCTION

1.1 G1000 CONTROLS

Figure 1-1 G1000 Controls

1.2 SECURE DIGITAL CARDS

1.3 SYSTEM POWER-UP

PFD Power Up

MFD Power Up

Figure 1-2 G1000 Power-Up

1.4 INITIAL OPERATIONS

1.5 BACKLIGHTING

1.6 REVERSIONARY MODE

Figure 1-3 G1000 Normal Mode

Figure 1-4 G1000 Reversionary Mode: Failed PFD

Figure 2-1 Default PFD Information

Figure 2-2 Additional PFD Information

2.1 BACKLIGHTING

Figure 2-3 PFD Setup Menu

2.2 SOFTKEY FUNCTION

Figure 2-4 PFD Softkeys (1 of 2)

Figure 2-4 PFD Softkeys (2 of 2)

2.3 FLIGHT INSTRUMENTS

Airspeed Indicator

Figure 2-5 Airspeed Indicator

Speed Ranges

Speed Indication

Speed Ranges

Figure 2-6 Red Pointer at Vne

Airspeed Trend Vector

Vspeed References

True Airspeed Box

Attitude Indicator

Pitch Indication

Figure 2-7 Attitude Indicator

Roll Indication

Figure 2-8 Attitude Indicator Nose High

Figure 2-9 Attitude Indicator Nose Low

Slip/Skid Indication

Altimeter

Altitude Reference Bug

Altitude Reference Bug

Altitude Trend Vector

Altitude Reference Box

Barometric Setting Box

Figure 2-10 Altimeter

Altitude Values

Altitude Alerting

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

Metric Display

Vertical Deviation/Glideslope Indicator

Marker Beacon Annunciations

Figure 2-14 Altimeter (Metric)

Figure 2-16 Marker Beacon and Vertical Deviation

Vertical Speed Indicator

Vertical Speed Pointer

Figure 2-16 Vertical Speed Indicator

Horizontal Situation Indicator

Figure 2-17 ARC HSI

Figure 2-18 Horizontal Situation Indicator

Heading Indication

Turn Rate Indicator

Course Deviation Indicator

Figure 2-21 Selected Course Box

Figure 2-20 Turn Rate Indicator and Trend Vector

Bearing Pointers and Information Windows

Figure 2-22 HSI with Bearing Information

Figure 2-24 BRG2 Information Window

Navigation Source

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