Garmin Software Version 0500.00- User Manual

Garmin Software Version 0500.00

Garmin Software Version 0500.00– 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 3 – Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58; Garmin
  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 8 – This page intentionally left blank.
  • Page 9 – vii; TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW
  • Page 10 – viii; SECTION 7: NAVIGATION
  • Page 11 – ix; SECTION 10: HAZARD AVOIDANCE
  • Page 12 – INDEX
  • Page 13 – SECTION 1; The purpose of this Cockpit Reference Guide is; The pilot should read and thoroughly
  • Page 14 – MFD Only
  • Page 16 – Softkey OFF
  • Page 17 – Figure 1-3 PFD Softkey Flow Chart – 1; METRIC
  • 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 following; The; OBS; softkey is only displayed when
  • 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
  • Page 31 – TRANSPONDER; The Nav/Com controls and frequency windows are
  • 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
  • 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; AP DISC (Autopilot Disconnect) Button; 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; If the Selected Altitude is captured during; CWS; button after the Selected Altitude is
  • 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 procedures; 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
  • 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; The following discussions pertain to the Multi-function; 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; 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; ACTIVATE A FLIGHT PLAN LEG
  • Page 73 – 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; CREATE A NEW FLIGHT PLAN
  • Page 74 – Figure 8-10 Create FPL on MFD; LOAD A DEPARTURE
  • Page 75 – Figure 8-13 Store Flight Plan Confirmation
  • Page 76 – Figure 8-15 Invert Flight Plan; COPY A FLIGHT PLAN; ABOVE
  • Page 77 – Figure 8-16 Trip Planning Page; : An active flight plan or Direct-to must be; NOTE; : VNAV is advisory only and cannot be
  • Page 79 – MAP; same; VNAV Page Menu Options; MENU
  • Page 81 – 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 82 – Figure 9-4 Select Arrival Transition; Load and/or Activate an Approach Procedure; Figure 9-6 Selecting an Approach Procedure
  • Page 83 – Figure 9-7 Selecting an Approach Transition; large FMS; Activate An Approach in the Active Flight Plan; PROC
  • Page 85 – SECTION 10 – HAZARD; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 86 – At a map range of less than 25 nm, Stormscope; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page
  • Page 87 – Use of XM weather for hazardous
  • Page 88 – Figure 10-9 Weather Data Link Page
  • Page 90 – Figure 10-10 Weather Product Symbols; The XM Information Page in the AUX Page Group will; The DONE softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
  • Page 91 – 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 seconds,; Figure 10-11 Traffic Map Page; Displaying Traffic on the Navigation Map; alert “Traffic” is given.
  • Page 92 – SKYWATCH TRAFFIC ADVISORY; Refer to the SkyWatch pilot’s guide for a detailed; Figure 10-12 Traffic Map Page
  • Page 93 – Figure 10-13 TAS Traffic on Navigation Map; Traffic Advisory; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Color
  • Page 94 – Figure 10-15 Obstacle Symbols; Displaying Terrain on the TAWS Page
  • Page 95 – Black; Enable/Disable Aviation Data; While the TAWS Page is displayed, press the; Figure 10-19 TAWS Page Menu
  • Page 96 – TAWS System; Enroute
  • Page 97 – Figure 10-20 Non-Precision Approach PDA Alert Threshold; CAUTION; Figure 10-21 ILS Approach PDA Alert Threshold; Figure 10-22 Excessive Descent Rate
  • Page 98 – Don’t Sink; “Five-Hundred” Aural Alert; With the Navigation Map displayed, press the; softkey. Terrain and obstacle; Figure 10-23 TAWS Symbols
  • Page 99 – When a terrain or obstacle alert is issued, a pop-up
  • Page 100 – Alert Type
  • Page 101 – The following system status annunciations may also be; Alert Annunciations; Figure 10-26 Alert Annunciation on the TAWS Page; Alert Annuciation; Figure 10-27 Alert Annunciation on the PFD
  • Page 102 – AIRBORNE WEATHER RADAR; Displaying Weather on the Weather Radar Page; Begin transmitting only when it is; Adjusting Antenna Tilt; Figure 10-28 Horizontal Scan Display
  • Page 103 – Figure 10-30 Bearing Line on Horizontal Scan; Bearing Line; Figure 10-31 Vertical Scan Display
  • Page 104 – Changing the gain in weather mode; Ground Mapping
  • Page 105 – Figure 10-34 Selecting Sector Scan Position; Antenna Stabilization; This feature is used as a tool to determine areas
  • Page 106 – To activate or deactivate the Watch feature, press the; WATCH; Figure 10-36 Horizontal Scan Without WATCH; Areas of Attenuated
  • Page 107 – SECTION 11 – ABNORMAL; SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; Reversionary display mode can also be manually; The Beechcraft 58 Pilot’s Operating
  • Page 108 – ABNORMAL COM OPERATION; When a COM tuning failure is detected by the system,; UNUSUAL ATTITUDES; The PFD will ‘declutter’ when the aircraft enters an; Figure 11-2 Extreme Pitch Indication; STORMSCOPE OPERATION WITH; If heading is lost, strikes and/or cells must be cleared
  • Page 109 – SECTION 12 – ANNUNCIATIONS; ALERTS; The Beechcraft 58/G58 Pilot’s Operating
  • Page 110 – ALERT LEVEL DEFINITIONS; red
  • Page 111 – GEAR UP; CAUTION Annunciation; BUSES TIED; Alert Message; PFD FAN FAIL
  • Page 112 – The following AFCS alert annunciations appear in the; Condition; Figure 12-5 AFCS System Status Field; System Status Field
  • Page 114 – When an LRU or an LRU function fails, a large red; Traffic Voice Alerts; Voice Alert
  • Page 115 – System Annunciation
  • Page 116 – A red ‘X’ may be the result of an LRU or an LRU; Figure 12-6 G1000 System Failure Annunciations; This section describes various G1000 system alert; This section provides information
  • Page 117 – Message
  • Page 118 – Alerts Window Message
  • Page 119 – GIA 63 Alert Messages
  • Page 121 – GEA 71 Alert Messages
  • Page 122 – GRS 77 Alert Messages
  • Page 125 – BACKUP PATH
  • Page 127 – Signal augmentation 5-2
  • Page 128 – Manual Electric Trim 6-1
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G1000

TM

Cockpit Reference Guide

for the Beechcraft 58/G58

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Summary

Page 3 - Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58; Garmin

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58 Copyright © 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0500.00 or later for the Beechcraft 58/G58. Some differences in opera-tion may be observed when comparing...

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58 v RECORD OF REVISIONS Part Number Change Summary 190-00526-00 Initial release. Revision Date of Revision Affected Pages Description A 10/3/05 i-Index-4 Initial release

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Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58 vi RECORD OF REVISIONS This page intentionally left blank.

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