Garmin Software Version 0458.01- User Manual

Garmin Software Version 0458.01

Garmin Software Version 0458.01– User Manual, read for free online in PDF format. We hope this helps you resolve any issues you may have. If you have further questions, please contact us through the contact form.

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Table of Contents:

  • Page 2 – Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36; or later for the Beechcraft A36/G36. Some differences in
  • Page 6 – This page intentionally left blank.
  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 9 – vii; TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW
  • Page 10 – viii; SECTION 7: NAVIGATION
  • Page 11 – ix; SECTION 10: HAZARD AVOIDANCE
  • Page 13 – SECTION 1; The purpose of this Cockpit Reference Guide is to; The pilot should read and thoroughly
  • Page 14 – MFD Only
  • Page 16 – Softkey OFF
  • Page 17 – Figure 1-3 PFD Softkey Flow Chart – 1; STD BARO – Press to set the barometric pressure
  • Page 18 – Figure 1-5 PFD Softkey Flow Chart – 3
  • Page 19 – Figure 1-6 MFD Softkeys
  • Page 20 – Figure 1-7 Page Group Icon
  • Page 21 – SECTION 2; SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 22 – Figure 2-2 Additional PFD Information; Next Waypoint
  • Page 23 – AIRSPEED INDICATOR; Figure 2-4 Airspeed Indicator; Speed Indication; Figure 2-5 Red Pointer at Vne; Speed Ranges; ON; ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator
  • Page 24 – Figure 2-7 Altimeter; Altitude Reference Bug; To set the altitude reference bug:; Altitude Trend Vector; BARO; INDICATOR; Figure 2-8 Marker Beacon and Vertical Deviation
  • Page 25 – VERTICAL SPEED INDICATOR; Figure 2-9 Vertical Speed Indicator; Vertical Speed Pointer; VS; HORIZONTAL SITUATION INDICATOR; Figure 2-10 Horizontal Situation Indicator
  • Page 26 – Figure 2-14 Turn Rate Indicator and Heading Trend Vector; Course Pointer; Figure 2-15 Course Pointer; Bearing Pointers and Information Windows; PFD; Figure 2-14 HSI with Bearing Information
  • Page 27 – To display the DME Information Window, press the; Figure 2-17 DME Information Window; Navigation Source; When using GPS as the navigation source, the follow-
  • Page 29 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; Figure 3-1 Default Engine Page; LEAN ENGINE DISPLAY; Figure 3-2 LEAN Engine Page
  • Page 30 – ENGINE SYSTEM DISPLAY; If desired, use the; Fuel calculations do not use the aircraft; Any exceedance of default Engine Page parameters,
  • Page 31 – TRANSPONDER; The Nav/Com controls and frequency windows are lo-
  • Page 32 – Figure 4-2 Frequency Fields
  • Page 33 – RADIO STATUS INDICATIONS; TX; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME; Figure 4-7 Radio Tuning Window; To change the DME tuning source:; Figure 4-8 DME Selection Window
  • Page 34 – Figure 4-10 Ground Mode
  • Page 35 – Following is a list of important codes:; Flight ID Reporting; If so configured, the Flight ID may be entered in the
  • Page 37 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 38 – COM RADIO SELECTION; COM1 MIC; Figure 5-2 Transceivers; MARKER BEACON RECEIVER; Figure 5-3 Marker Beacon Signal Indicator Lights on the PFD; Marker Beacon Signal Sensitivity; HI SENS; Figure 5-4 Marker Beacon; NAV RADIO AUDIO SELECTION
  • Page 39 – Figure 5-5 Navigation Radios; INTERCOM SQUELCH CONTROL
  • Page 40 – DIGITAL CLEARANCE RECORDER; PLAY
  • Page 41 – SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; FD; Figure 6-2 Command Bars; MODE ANNUNCIATIONS
  • Page 42 – Figure 6-3 PFD AFCS Display; OVERSPEED PROTECTION; Figure 6-4 Overspeed Annunciation; AP; Figure 6-5 Autopilot Engaged Annunciation
  • Page 43 – Automatic Disconnect; Manual Disengagement; Manual Disconnect; Control Wheel Steering; Yaw Damper; Yaw Damper is active.; PITCH AXIS MODES
  • Page 44 – AFCS Key; Figure 6-12 Pitch Hold Mode
  • Page 45 – ALT; Figure 6-13 Altitude Hold Mode; CWS
  • Page 46 – Figure 6-14 Vertical Speed Hold Mode
  • Page 47 – Figure 6-15 Flight Level Change Mode
  • Page 48 – Pressing the
  • Page 49 – Mode annunciations for active roll axis modes are; Figure 6-17 Roll Hold Mode
  • Page 50 – Figure 6-18 Heading Select Mode; HDG
  • Page 51 – NAV; When making a backcourse approach, set; Navigation Mode Armed
  • Page 52 – The Approach mode acquires and tracks the selected; The Glideslope mode is automatically; See the Example Procedures Using AFCS section for
  • Page 53 – EXAMPLE PROCEDURES USING AFCS; This section provides a scenario-based set of proce-; Figure 6-21 Flight Plan Overview
  • Page 54 – Figure 6-22 Departure
  • Page 55 – After climbout, the autopilot continues to fly the aircraft; CDI; Figure 6-23 Intercepting a VOR
  • Page 56 – The aircraft is currently tracking inbound on the; Figure 6-24 Transition to GPS Flight Plan; key to reactivate the auto-
  • Page 57 – In preparation for the approach to KFAT, set; key. ‘FLC’ is annunciated; Figure 6-25 FLC Descent; As the aircraft reaches the selected altitude,
  • Page 58 – Figure 6-26 ILS Approach to KFAT
  • Page 61 – SECTION 7 – NAVIGATION; NAVIGATION MAP PAGE; Select the MAP Page Group; The map display should only be; Direct-to Navigation from the MFD
  • Page 62 – Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 63 – AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page; knob to select the ‘WPT’ page; Access Runway Information; key
  • Page 64 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Access Information on an Intersection; Figure 7-7 NDB Information Page; Select the NDB Information Page
  • Page 65 – Figure 7-8 VOR Information Page; Select the VOR Information Page; USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on cre-; NEAREST AIRPORTS; Figure 7-9 Nearest Airports Page; Nearest Airport Information on the MFD
  • Page 66 – Figure 7-10 Nearest Airports Window; NEAREST INTERSECTIONS; Figure 7-11 Nearest Intersections Page; Select the Nearest Intersections Page
  • Page 67 – Figure 7-12 Nearest NDB Page; Select the Nearest NDB Page; Figure 7-13 Nearest VOR Page; View Information on the Nearest VOR:
  • Page 68 – NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page; NEAREST FREQUENCIES; Figure 7-15 Nearest Frequencies Page; Select the Nearest Frequencies Page
  • Page 69 – NEAREST AIRSPACES; Figure 7-16 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an; View Additional Details for a Listed Airspace
  • Page 71 – SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page
  • Page 72 – VIEWING THE ACTIVE FLIGHT PLAN; Figure 8-2 Active Flight Plan Page on the MFD; ACTIVATE A STORED FLIGHT PLAN; Figure 8-4 Flight Plan Catalog Page
  • Page 73 – ACTIVATE A FLIGHT PLAN LEG; Figure 8-5 Activate Flight Plan Leg Confirmation; STOP NAVIGATING A FLIGHT PLAN; Figure 8-6 Delete Flight Plan; INVERT ACTIVE FLIGHT PLAN; Figure 8-8 Invert Flight Plan
  • Page 74 – Figure 8-9 Invert Flight Plan Confirmation; CREATE A NEW FLIGHT PLAN; Figure 8-10 Create FPL on MFD; Create a new flight plan using the PFD; A flight plan cannot be entered using the
  • Page 75 – Figure 8-13 Store Flight Plan Confirmation
  • Page 76 – Figure 8-14 Remove Waypoint Confirmation; INVERT AND ACTIVATE A STORED; Figure 8-15 Invert Flight Plan; COPY A FLIGHT PLAN; ABOVE
  • Page 77 – Figure 8-16 Trip Planning Page
  • Page 79 – SECTION 9 – PROCEDURES; SECTION 9: PROCEDURES; ARRIVALS AND DEPARTURES; Load and Activate a Departure Procedure; Figure 9-1 Select Departure; Load and Activate An Arrival Procedure; Figure 9-3 Select Arrival
  • Page 80 – Figure 9-4 Select Arrival Transition; Load and/or Activate an Approach Procedure; Figure 9-6 Selecting an Approach Procedure
  • Page 81 – Figure 9-7 Selecting an Approach Transition; large FMS; Activate An Approach in the Active Flight Plan; PROC
  • Page 83 – SECTION 10 – HAZARD; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 84 – At a map range of less than 25 nm, Stormscope light-; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page
  • Page 85 – “Cell mode” uses a clustering program to
  • Page 86 – Figure 10-8 METAR and TAF Text Displayed on the; NEXRAD
  • Page 87 – Strikes depicted represent cloud to ground; joystick
  • Page 88 – key and; ENT; Weather Products and Symbols; Figure 10-10 depicts the symbol for each weather; Figure 10-10 Weather Product Symbols; Echo Top (Cloud Top and Echo Top Mutually Exclusive); Weather Product Age; The age for each of the enabled products is displayed
  • Page 89 – Weather Product; TRAFFIC INFORMATION SERVICE; If the G1000 is configured to use the; Displaying Traffic on the Traffic Map Page; If data is not received for a period longer than 6 sec-; Figure 10-11 Traffic Map Page
  • Page 90 – alert “Traffic” is given.; SKYWATCH TRAFFIC ADVISORY; Refer to the SkyWatch pilot’s guide for a detailed dis-; Figure 10-12 Traffic Map Page; Displaying Traffic on the Navigation Map
  • Page 91 – Figure 10-13 TAS Traffic on Navigation Map; Traffic Advisory; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Color
  • Page 92 – Figure 10-15 Obstacle Symbols
  • Page 93 – SECTION 11 – ABNORMAL; SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either dis-; Normal PFD Display; Reversionary display mode can also be manually ac-; The Beechcraft A36/G36 Pilot’s Operating
  • Page 94 – ABNORMAL COM OPERATION; When a COM tuning failure is detected by the system,; UNUSUAL ATTITUDES; The PFD will ‘declutter’ when the aircraft enters an un-; Figure 11-2 Extreme Pitch Indication; STORMSCOPE OPERATION WITH; If heading is lost, strikes and/or cells must be cleared
  • Page 95 – SECTION 12 – ANNUNCIATIONS; ALERTS
  • Page 96 – ALERT LEVEL DEFINITIONS; red
  • Page 97 – The following alert annunciations are configured; WARNING Annunciation; GEAR UP; CAUTION Annunciation; AC DOOR EXTD; ADVISORY Annunciation; BUSES TIED; Alert Message; PFD FAN FAIL
  • Page 98 – The following AFCS alert annunciations appear in the; Condition; Figure 12-5 AFCS System Status Field; System Status Field
  • Page 99 – When an LRU or an LRU function fails, a large red ‘X’ is; Voice Alerts; Voice Alert
  • Page 100 – System Annunciation
  • Page 101 – A red ‘X’ may be the result of an LRU or an LRU func-; Figure 12-6 G1000 System Failure Annunciations; This section describes various G1000 system alert mes-; This section provides information regard-
  • Page 102 – Message
  • Page 103 – Alerts Window Message
  • Page 104 – GIA 63 Alert Messages
  • Page 106 – GEA 71 Alert Messages
  • Page 107 – GRS 77 Alert Messages
  • Page 108 – HDG FAULT; GDL 69 Alert Messages; GDC1 CONFIG
  • Page 110 – BACKUP PATH
  • Page 111 – INDEX; Signal augmentation 5-2
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G1000

TM

Cockpit Reference Guide

for the Beechcraft A36/G36

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Summary

Page 2 - Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36; or later for the Beechcraft A36/G36. Some differences in

Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36 Copyright © 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0458.0 1 or later for the Beechcraft A36/G36. Some differences in operation may be observed when compari...

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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36 iv WARNINGS, CAUTIONS, & NOTES This page intentionally left blank.

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36 v RECORD OF REVISIONS Part Number Change Summary 190-00525-00 Initial release. Revision Date of Revision Affected Pages Description A 7/05 i-Index-4 Initial release

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