Garmin Software Version 0424.01- User Manual

Garmin Software Version 0424.01

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Table of Contents:

  • Page 2 – Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
  • Page 3 – COPYRIGHT; Garmin
  • Page 4 – RECORD OF REVISIONS; Revision Date of Revision Affected Pages
  • Page 5 – TABLE OF CONTENTS
  • Page 6 – Section 4: Multi Function Display
  • Page 7 – Appendix A; A.3 Mooney Specific Aircraft Alerts; Index
  • Page 8 – LIST OF FIGURES
  • Page 10 – LIST OF TABLES; Table 3-1 Marker Beacon Signal Characteristics
  • Page 11 – WARRANTY; LIMITED WARRANTY; FROM
  • Page 12 – Pilots using an outdated database do so entirely at their own risk
  • Page 13 – CAUTION
  • Page 14 – This page intentionally left blank.
  • Page 15 – SECTION 1 – INTRODUCTION; SECTION 1: INTRODUCTION; It is not intended to be a; The pilot should read and thoroughly
  • Page 18 – SECURE DIGITAL CARDS; To install an SD card:; Press the card into place until it seats on the; To remove an SD card:; Gently press on the card to release the spring; Appendix A of the G1000 Pilot’s Guide
  • Page 19 – As the G1000 system begins to initialize, test annun-; MFD Power Up; The MFD Power-up Page displays general information
  • Page 20 – INITIAL OPERATIONS; ENT; REVERSIONARY MODE; NOTE: The system alerts the pilot when backup
  • Page 21 – Figure 1-4 G1000 Reversionary Mode: Failed PFD
  • Page 23 – SECTION 2 – PFD; SECTION 2: PRIMARY FLIGHT; This Cockpit Reference Guide describes the basic fea-; In the event that the airspeed,; The PFD displays the following:
  • Page 24 – Figure 2-1 Default PFD Information
  • Page 25 – Figure 2-2 Additional PFD Information
  • Page 26 – The backlighting of the display and the keys can be; Except in reversionary mode, the back-; MENU; key is pressed to change the backlighting.
  • Page 27 – SOFTKEY FUNCTION; Softkey Off
  • Page 31 – FLIGHT INSTRUMENTS; Airspeed Indicator; Figure 2-5 Airspeed Indicator; Speed Indication; Figure 2-6 Red Pointer at Vne; Airspeed Trend Vector
  • Page 32 – Figure 2-7 Attitude Indicator; Pitch Indication
  • Page 33 – Figure 2-8 Attitude Indicator Nose High; Roll Indication; Major tick marks at 30 and 60 degrees and minor tick; NOTE; : Supplemental flight data such as the Inset; The Slip/Skid indicator resides beneath the roll pointer.
  • Page 34 – Figure 2-10 Altimeter
  • Page 35 – Altitude Alerting; Altitude alerting provides the pilot with a visual and; Figure 2-11 Colors Associated with the Altitude Alerter
  • Page 36 – Metric Display; Reference and current altitude can be displayed in me-; PFD; softkey to display the second; METRIC; softkey to display altitude in; BACK; softkey to return to the top level; Vertical Deviation/Glideslope Indicator; The Vertical Deviation/Glideslope Indicator is a win-; Marker Beacon Annunciations; Marker Beacon Annunciations are displayed on the; Figure 2-16 Marker Beacon and Vertical Deviation; Marker Beacon
  • Page 37 – The Vertical Speed Indicator displays the aircraft verti-; Vertical Speed Pointer; The Vertical Speed Pointer displays the current vertical; Digits appear in the pointer when the; Vertical Speed
  • Page 38 – Lateral Deviation; Figure 2-18 Horizontal Situation Indicator
  • Page 39 – Heading Indication; A digital reading of the current magnetic heading ap-; Figure 2-19 Selected Heading Box; Turn Rate Indicator; The Turn Rate Indicator resides directly above the ro-; Figure 2-20 Turn Rate Indicator and Trend Vector; Course Deviation Indicator; Figure 2-21 Selected Course Box; The CDI has angular limits exactly the same as a me-
  • Page 40 – Bearing Pointers and Information Windows; There are 2 bearing pointers available, 1 or 2 can be; Figure 2-22 HSI with Bearing Information; Figure 2-24 BRG2 Information Window
  • Page 41 – The HSI can display two sources of navigation, GPS
  • Page 42 – SURVEILLANCE; Communication Frequency Window; The Communication Frequency window provides the; Operating procedures for the Communica-; Navigation Frequency Window; The Navigation Frequency window provides the con-; Operating procedures for the Navigation Fre-
  • Page 43 – The Navigation Status Bar resides at the top of the PFD; : The fields in the PFD Navigation Status
  • Page 44 – Transponder Operation; Figure 2-30 Transponder Status Bar; ALERTS AND ANNUNCIATIONS
  • Page 45 – SECTION 3 – AUDIO PANEL; SECTION 3: AUDIO PANEL; : A complete audio panel description with; N OT E; : R e f e r t o t h e A u d i o Pa n e l P i l o t ’s; FRONT PANEL CONTROLS
  • Page 46 – Figure 3-1 Front Panel Controls
  • Page 47 – pressed to open the selected output channel.; Unmuted/Unswitched Inputs; ALT warning
  • Page 48 – COM MIC; Lighting
  • Page 49 – A PTT switch must be pressed to allow; Pressing a COM MIC Key; Audio level of the selected COM radio(s)
  • Page 50 – : Split COM performance varies significantly; PA Function; PA volume is adjustable in Configuration
  • Page 51 – Only the copilot; can make PA announce-; Speaker Output; SPKR
  • Page 52 – MARKER BEACON RECEIVER; Description and Operation; audio muting capability; The marker beacon receiver lights operate; Marker Beacon Signal Augmentation; HI SENS; Figure 3-4 Marker Beacon
  • Page 53 – Beacon; per minute
  • Page 54 – DME; Figure 3-6 Aircraft Radios
  • Page 55 – Table 3-2 ICS Isolation Mode Transitions; CREW Mode
  • Page 56 – Selected radios pilot; Table 3-3 ICS Operation Modes; When the; MAN SQ; is automatically annunci-
  • Page 58 – VOL; annunciation is lit, press the; annunciation, and; SQ; annunciation is already lit, turn the; DISPLAY BACKUP MODE; Pressing the red; Figure 3-8 Reversionary Mode
  • Page 59 – SECTION 4 – MFD; SECTION 4: MULTI FUNCTION
  • Page 60 – Figure 4-2 MFD Softkeys
  • Page 61 – ENGINE INDICATION SYSTEM; ENGINE Page; Manifold Pressure Gauge; : The Fuel Quantity Indicator will only dis-; : The pilot should refer to the Aircraft Flight
  • Page 63 – Th e L e a n a n d S y s t e m p a g e s a r e
  • Page 64 – The MFD displays GPS/Navigation flight information; To select a specific page group:; knob until the desired page; Figure 4-5 Page Group Window; To select a different page within the group:; Figure 4-6 Page Title Window
  • Page 65 – CLR; : Data is entered using the large and small; small or large FMS; Pressing the softkeys does not; Figure 4-6 Menu With Options
  • Page 66 – NAVIGATION MAP PAGE; WARNING; : The Navigation Map page display; knob to select the Map Page; : In addition to turning the; Navigation Map Page Operations
  • Page 67 – Figure 4-8 Navigation Map Page
  • Page 68 – Changing the Map Orientation; : A complete list of available map datums; Selecting a Map Range; Map; Figure 4-9 Navigation Map Range; Using the Auto Zoom Feature
  • Page 69 – The Navigation Map Page can be quickly decluttered; : “SUA” listed in the table below stands; Map panning moves the map beyond its current limits; : The airspace boundary stays highlighted; to display the panning
  • Page 70 – Figure 4-10 Navigation Map Panning
  • Page 71 – The Navigation Map Page displays various shades of; TRAFFIC softkey; Figure 4-11 TRAFFIC, TOPO and TERRAIN Softkeys; Pressing the; : Traffic and terrain data can also be
  • Page 72 – P r e s s t h e; Pressing the; The Navigation Map Page displays cell or strike; softkey. Press the
  • Page 73 – In normal operation, the current mode and rate; MFD Navigation Status Window; The MFD Navigation Status Window displays four,; Figure 4-13 MFD Navigation Status Window; : Instructions on changing a data field on
  • Page 74 – Figure 4-14 Navigation Map Page Menu Options
  • Page 75 – TRAFFIC MAP PAGE; The Traffic Map Page displays the following informa-; To select the Traffic Map Page:; Select the MAP group of pages. Turn the; small; knob to select the Traffic Map Page.; : TIS warns the pilot with voice and
  • Page 76 – Figure 4-15 Traffic Map Page
  • Page 77 – Item; Traffic Map Page Operations; Changing the Map Range; Turn the joystick clockwise to zoom out, or turn; available in all areas.
  • Page 78 – The TIS Traffic Advisory (TA) should alert
  • Page 79 – TIS Traffic Status; The MFD indicates the following TIS traffic status to; Traffic Banner; • AGE - if traffic data is not refreshed within 6
  • Page 80 – WEATHER MAP PAGE; The G1000 provides an optional display interface for the; : Refer to the WX-500 User’s Guide for a; Range; The Weather Map Page displays the following
  • Page 81 – : The WX-500 has to be receiving valid; For weather display interpretation, the examples in the; Weather Map Page Operations; The following Weather Map Page operations can be; : An active flight plan or Direct-to is
  • Page 82 – TERRAIN PROXIMITY PAGE; CAUTION: Terrain and obstacle data are provided; The Terrain Proximity Page displays the following:; Figure 4-17 Terrain Scale; Terrain Proximity Page Operations; There are two terrain/obstacle viewing options avail-
  • Page 83 – The Terrain Proximity Page displays obstacle data; Obstacle; Obstacle Shapes; The Map Setup Page Menu has ‘OBSTACLE’ and; TERRAIN PROXIMITY PAGE; Note: Obstacles are only displayed at certain map
  • Page 84 – The “Direct-to” function provides a quick method of; small FMS; If navigating to a waypoint and the aircraft moves off
  • Page 85 – In addition to selecting a Direct-to waypoint using an; : the G1000s Spell N Find feature selects; Any waypoint contained in the flight plan may be se-; Figure 4-19 Flight Plan Waypoint Direct-to
  • Page 86 – The following are “candidates” for Direct-to way-
  • Page 87 – Canceling Direct-to Navigation; Once a direct-to is activated, the G1000 provides; key to display the direct-to; key. If a flight plan is still active, the
  • Page 88 – When Direct-to is activated, the G1000 sets a direct
  • Page 90 – large FMS; Figure 4-22 New Flight Plan
  • Page 91 – Figure 4-23 Remove Waypoint Confirmation
  • Page 92 – Figure 4-24 Removing an Approach; FLIGHT PLAN CATALOG PAGE; The Flight Plan Catalog Page is the second flight planning; Flight Plans; Figure 4-25 Flight Plan Catalog Page
  • Page 93 – The following operations can be performed from the; Figure 4-26 Flight Plan Catalog Page Options; Once a flight plan is defined using the Flight Plan; Figure 4-27 Activate Stored Flight Plan Confirmation
  • Page 94 – Figure 4-28 Delete Flight Plan Confirmation; ‘Invert & Activate FPL’ allows the active flight plan to
  • Page 95 – ‘Delete All’ removes all flight plans from memory at
  • Page 96 – Based upon the active flight plan or Direct-to desti-; Figure 4-29 Procedures Page
  • Page 97 – The G1000 allows you to fly non-precision and pre-; G1000 Navigational Guidance for Approaches; The G1000 supports all ARINC 424 leg types that have; : The G1000 does not provide steering guid-; : The pilot is responsible for determining; : The approach charts shown in this section
  • Page 98 – In order to select an approach, there must be an active; Figure 4-30 Selecting an Approach Procedure
  • Page 99 – Not all approaches in the database are approved for; To activate an Approach Procedure:; With an approach loaded in the active flight; PROC; key to display the Proce-; knob to highlight ‘Activate; Figure 4-32 Activating an Approach Procedure; : The G1000 is designed to complement; : The GPS approach examples given in
  • Page 100 – An approach where there is no procedure turn re-; : When the message ‘RAIM is not avail-
  • Page 101 – Figure 4-33 Approach with No Procedure Turn
  • Page 102 – As you pass the MAP, and the runway is not in view, a
  • Page 103 – Figure 4-34 Flying the Missed Approach
  • Page 104 – The procedure turn portion of the approach is stored
  • Page 105 – As the pilot approaches the MAP, a waypoint; SUSP; softkey to initiate the missed approach; Figure 4-35 Flying the Procedure Turn; : Once you cross the FAF, the final course
  • Page 106 – Flying the DME ARC; The GPS overlay for a DME arc approach uses ad-
  • Page 107 – Figure 4-36 Flying the DME Arc and Vectors to the DME Arc
  • Page 108 – This example is based upon a missed approach from
  • Page 109 – Upon crossing the MAP, ‘SUSP’ appears on the; softkey to initiate the; Figure 4-37 Flying a Holding Pattern; : Remember do not press the OBS softkey
  • Page 111 – APPENDIX A; IMPORTANT NOTE; : The Aircraft Flight Manual
  • Page 112 – The G1000 Alerting System uses a single alert level for; Figure A-2 ADVISORY Softkey
  • Page 113 – A.3 MOONEY SPECIFIC AIRCRAFT ALERTS; The following information is configured specifically; Audio Alerts; Audio Alert; : Audio and Voice Alerts are provided to; Voice Alerts; The following voice alerts can be configured to be
  • Page 114 – When an LRU or an LRU function fails, a large red; IMPORTANT NOTE
  • Page 115 – System Annunciation
  • Page 116 – A red ‘X’ may be the result of an LRU or an LRU func-; Figure A-3 G1000 System Failure Annunciations
  • Page 117 – A.5 G1000 SYSTEM MESSAGE ADVISORIES; This section describes various G1000 system message; MFD & PFD Message Advisories; Message
  • Page 118 – GMA 1347 Message Advisories; Alerts Window Message
  • Page 122 – GMU 44 Message Advisories
  • Page 123 – Miscellaneous Message Advisories
  • Page 125 – INDEX; Jeppesen x
  • Page 126 – Navigation Map Page Options Menu
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G1000

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cockpit reference guide

for Mooney M20M & M20R

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Summary

Page 2 - Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R

Page 3 - COPYRIGHT; Garmin

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R i COPYRIGHT Copyright © 2004 Garmin Ltd. or its subsidiaries. All rights reserved. This Cockpit Reference Guide reflects the operation of System Software version 0424.01 for Mooney M20M and M20R aircraft. Some differences in operation ma...

Page 4 - RECORD OF REVISIONS; Revision Date of Revision Affected Pages

Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R ii RECORD OF REVISIONS Revision Date of Revision Affected Pages Description ECO Number A B 10/19/04 11/02/24 i - xii, 1 - 114 i - xii, 1 - 114 Production Release Update SW number. 27851 28077

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