Garmin Software Version 0552.00- User Manual

Garmin Software Version 0552.00

Garmin Software Version 0552.00– 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 Quest Kodiak 100
  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 8 – Blank Page
  • Page 9 – TABLE OF CONTENTS
  • Page 10 – ii; SECTION 8: FLIGHT PLANNING
  • Page 11 – iii; SECTION 11: ABNORMAL OPERATION
  • Page 13 – SECTION 1; SECTION 1: SYSTEM OVERVIEW; The purpose of this Cockpit Reference Guide is; The pilot should read and thoroughly
  • Page 16 – Softkey OFF; INSET; Figure 1-3 INSET Softkeys
  • Page 17 – PFD; Figure 1-4 PFD Configuration Softkeys; METRIC
  • Page 19 – Figure 1-6 MFD Softkeys
  • Page 20 – Figure 1-7 Page Group Icon
  • Page 21 – DATABASE UPDATES; Aviation Database Update; Figure 1-9 Database Update Prompt; ENT; Figure 1-10 Database Update Confirmation; Terrain and Obstacle Database Updates; These databases are not stored internally in the MFD; TOPO
  • Page 22 – Figure 1-11 Power-Up Splash Screen Window
  • Page 23 – SECTION 2; SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 24 – Figure 2-2 Additional PFD Information; Next Waypoint
  • Page 25 – 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 26 – Figure 2-7 Altimeter; Altitude Select Bug; To set the Selected Altitude Bug:; Turn the; Knobs to set the Altitude Select; ALT; Knob sets the hundreds and; ALT; Knob sets the thousands. This; Altitude Trend Vector; BARO; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Barometric Minimum Descent Altitude
  • Page 27 – Figure 2-9 Barometric Minimum Descent Altitude; INDICATOR; The Vertical Deviation/Glideslope Indicator appears; MARKER BEACON ANNUNCIATIONS; Figure 2-10 Marker Beacon and Vertical Deviation; VERTICAL SPEED INDICATOR; Figure 2-11 Vertical Speed Indicator; The actual vertical speed is displayed inside the
  • Page 28 – HORIZONTAL SITUATION INDICATOR; Arc HSI; When the Arc HSI is displayed the BRG1; • Localizer – Diamond; Lateral; Turn Rate Indicator and Heading Trend Vector
  • Page 29 – Figure 2-15 Standard-Rate Turn Indication; Course Pointer; Figure 2-16 Course Pointer; Bearing Pointers and Information Windows; Figure 2-17 HSI with Bearing Information
  • Page 30 – Figure 2-19 BRG2 Information Window; Navigation Source; When using GPS as the navigation source, the following; The; OBS; Softkey is only displayed when
  • Page 31 – SECTION 3 – EICAS; SECTION 3: ENGINE INDICATION; Engine Display; ENGINE; Figure 3-1 Kodiak Default Engine Display; Engine System Display; SYSTEM; Figure 3-2 Kodiak SYSTEM Engine Display
  • Page 32 – Fuel calculations do not use the aircraft; FUEL; Figure 3-3 Kodiak FUEL Engine Display
  • Page 33 – TRANSPONDER; The Nav/Com controls and frequency boxes are located
  • Page 34 – Figure 4-2 Frequency Fields
  • Page 35 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; Auto-tuning on the PFD; NRST; Auto-tuning on the MFD; FMS
  • Page 36 – TRANSPONDER OPERATION; Mode Selection; Figure 4-8 Ground Mode; Code Number and; Figure 4-9 Standby Mode; ON Mode; Figure 4-11 Altitude Mode; Reply Status; Figure 4-12 Reply Indication; Reply; Code Selection; The pre-programmed VFR Code is set at
  • Page 37 – ) P r e s s t h e; CODE; S o f t ke y t o d i s p l a y t h e; BKSP; Flight ID Reporting; If so configured, the Flight ID may be entered in the; Flight ID
  • Page 39 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Front Panel Controls
  • Page 40 – COM RADIO SELECTION; COM1 MIC; Figure 5-2 Transceivers; MARKER BEACON RECEIVER; MUTE; Figure 5-3 Marker Beacon Annunciators on the PFD; Marker Beacon Signal Sensitivity; HI SENS; Figure 5-4 Marker Beacon; NAV RADIO AUDIO SELECTION; Figure 5-5 Navigation Radios
  • Page 41 – PILOT; Figure 5-6 ICS Isolation; INTERCOM SQUELCH CONTROL; MAN SQ
  • Page 42 – DIGITAL CLEARANCE RECORDER; Figure 5-8 Clearance Recorder Play Key; PLAY; REVERSIONARY MODE; Figure 5-9 Reversionary Mode Button; DISPLAY BACKUP
  • Page 43 – SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FLIGHT; Refer to the pilot’s guide for the installed autopilot
  • Page 45 – SECTION 7 – NAVIGATION; 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 46 – Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 47 – AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page
  • Page 48 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Select the NDB Information Page
  • Page 49 – 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 50 – Figure 7-10 Nearest Airports Window
  • Page 51 – NEAREST INTERSECTIONS; Figure 7-11 Nearest Intersections Page; Select the Nearest Intersections Page; Figure 7-12 Nearest NDB Page; Select the Nearest NDB Page
  • Page 52 – Figure 7-13 Nearest VOR Page; NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page
  • Page 53 – NEAREST FREQUENCIES; Figure 7-15 Nearest Frequencies Page; Select the Nearest Frequencies Page; NEAREST AIRSPACES; Figure 7-16 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an
  • Page 55 – SECTION 8 – FLIGHT PLANNING; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page
  • Page 56 – VIEWING THE ACTIVE FLIGHT PLAN; Figure 8-2 Active Flight Plan Window on the PFD; ACTIVATE A STORED FLIGHT PLAN; Figure 8-4 Flight Plan Catalog Page
  • Page 57 – 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 58 – CREATE A NEW FLIGHT PLAN; Create a New Flight Plan Using the MFD; Figure 8-10 Create FPL on MFD; Create a New Flight Plan Using the PFD; A flight plan cannot be entered using the
  • Page 59 – Figure 8-13 Store Flight Plan Confirmation
  • Page 60 – INVERT AND ACTIVATE A STORED
  • Page 61 – Figure 8-15 Trip Planning Page; Starting WPT; The Page Mode must be set to MANUAL
  • Page 62 – An active flight plan or Direct-to must be; Create a Vertical Navigation Profile
  • Page 63 – 0) With the ‘TARGET ALTITUDE’ field highlighted,; Knobs to select; Key. The cursor is now placed; MAP; VNAV Page Menu Options; MENU
  • Page 65 – 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; If any portion of an arrival procedure is
  • Page 66 – Figure 9-3 Select Arrival; Not all approaches in the database are approved for GPS; Load and/or Activate an Approach Procedure
  • Page 67 – Figure 9-6 Selecting an Approach Procedure; Activate An Approach in the Active Flight Plan
  • Page 69 – SECTION 10 – HAZARD; SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 70 – 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 71 – Use of XM weather for hazardous
  • Page 72 – Figure 10-9 Weather Data Link Page
  • Page 74 – Figure 10-10 Weather Product Symbols; The XM Information Page in the AUX Page Group will; DONE; Softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
  • Page 75 – 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 76 – SKYWATCH TRAFFIC ADVISORY; Refer to the SkyWatch pilot’s guide for a detailed; Figure 10-12 Traffic Map Page
  • Page 77 – Figure 10-13 TAS Traffic on Navigation Map; Traffic Advisory; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Color
  • Page 78 – Figure 10-15 Obstacle Symbols; Displaying Terrain on the TAWS Page
  • Page 79 – Red; Enable/Disable Aviation Data; Figure 10-18 TAWS Page Menu; TAWS Inhibit; Flying VFR into an area where unique terrain exists
  • Page 80 – TAWS System; ) While the TAWS Page is displayed, press the; Enroute; Figure 10-19 PDA Alerting
  • Page 81 – Figure 10-20 Excessive Descent Rate; Negative Climb Rate After Takeoff; Don’t Sink; Figure 10-21 Negative Climb Rate; “Five-Hundred” Aural Alert
  • Page 82 – Displaying Terrain and Obstacles on the; ) With the Navigation Map displayed, press the; Softkey. Terrain and obstacle; Figure 10-23 TAWS Symbols; Alert Annunciations; Figure 10-24 Alert Annunciation on the TAWS Page; Alert Annunciation; Figure 10-25 Alert Annunciation on the PFD
  • Page 83 – Alert Type
  • Page 84 – The following system status annunciations may also be
  • Page 85 – 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 Quest Kodiak 100 Pilot’s Operating
  • Page 86 – When a COM tuning failure is detected by the system,; Figure 11-2 Extreme Pitch Indication; If heading is lost, strikes and/or cells must be cleared; Figure 11-3 Loss of Hazard Functions
  • Page 87 – SECTION 12 – ANNUNCIATIONS; ALERTS; The Airplane Flight Manual supersedes
  • Page 88 – ALERT LEVEL DEFINITIONS
  • Page 89 – AIRCRAFT ALERTS; See the Airplane Flight Manual for information; WARNING Alerts; CAUTION Alerts; Annunciation Window Text
  • Page 90 – FOD DOOR NRM; Message Advisory Alerts; GIA FAN FAIL
  • Page 91 – When an LRU or an LRU function fails, a large red
  • Page 92 – System Annunciation
  • Page 93 – A red ‘X’ may be the result of an LRU or an LRU; Figure 12-5 G1000 System Failure Annunciations; ADVISORIES; This section describes various G1000 system message; This Section provides information
  • Page 94 – Message
  • Page 95 – Database Message Advisories; Alerts Window Message
  • Page 96 – GMA 1347 Message Advisories
  • Page 100 – GMU 44 Message Advisories
  • Page 103 – TRAFFIC FAIL; – Traffic device has; STRMSCP FAIL; – Stormscope has; BACKUP PATH; – Stormscope using
  • Page 105 – INDEX; Signal augmentation 5-2
  • Page 108 – © 2007 Garmin Ltd. or its subsidiaries
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Integrated Flight Deck

Cockpit Reference Guide

Quest

Kodiak 100

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Summary

Page 3 - Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 Copyright © 2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0552.00 or later for the Quest Kodiak 100. Some differences in operation may be observed when comparing th...

Page 7 - RECORD OF REVISIONS; Part Number

190-00645-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00645-00 Initial release. Revision Date of Revision Affected Pages Description A March, 2007 i through Index-4 Production release

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190-00645-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 RR-2 RECORD OF REVISIONS Blank Page

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