Garmin Software Version 0648.02- User Manual

Garmin Software Version 0648.02

Garmin Software Version 0648.02– 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 Piper PA32
  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 8 – Blank Page
  • Page 9 – TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW
  • Page 10 – ii; SECTION 8: FLIGHT PLANNING
  • Page 11 – iii; SECTION 11: ABNORMAL OPERATION
  • Page 13 – SECTION 1; The purpose of this Cockpit Reference Guide is; The pilot should read and thoroughly
  • Page 16 – Softkey OFF; Figure 1-3 INSET Softkeys; INSET
  • Page 17 – Figure 1-4 PFD Configuration Softkeys; PFD
  • Page 18 – OBS; Figure 1-5 Transponder Softkeys; IDENT
  • Page 19 – ENGINE; Figure 1-6 MFD Softkeys; MAP
  • Page 20 – Turn the large; Knob until the desired page; FMS; Knob to select pages within; Figure 1-7 Page Group Icon; VERTICAL NAVIGATION; All arrival procedure altitudes contained in
  • Page 21 – White Text; Table 1-1 VNV Altitude Text Size and Color; CLR
  • Page 22 – Figure 1-8 VNV Altitudes; Some altitudes retrieved from the database have; Figure 1-9 Altitude Restrictions; See Section 7 - Navigation, for a sample flight plan; Figure 1-10 PFD Setup Menu Window; DATABASE UPDATES; The G1000 system uses Secure Digital (SD) cards to
  • Page 23 – After the aviation database is installed,; ENT; Key to start the database update.; Figure 1-12 Database Update Confirmation; Garmin Databases; Since these databases are not stored internally in the; The data contained in the terrain and
  • Page 24 – Figure 1-13 Power-Up Splash Screen Window; Creating a Profile
  • Page 27 – SECTION 2; SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 28 – Figure 2-2 Additional PFD Information; Active Flight Plan Leg
  • Page 29 – AIRSPEED INDICATOR; Figure 2-4 Airspeed Indicator; Speed Indication; Figure 2-5 Red Pointer; Airspeed Trend Vector; ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator
  • Page 30 – Figure 2-7 Altimeter; Altitude Reference Bug; The Altitude Reference Bug is displayed at the Selected; Altitude Trend Vector; The end of the trend vector displays approximately; Barometric Setting Box; Figure 2-8 Altitude Alerting Visual Annunciations; Visual annunciations appear in the Altitude Reference; Metric Display
  • Page 31 – GLIDESLOPE INDICATOR; VNV altitudes displayed on the Active; The Vertical Deviation and Required Vertical Speed; Figure 2-10 Vertical Deviation Indications; Figure 2-11 Glidepath Indicator
  • Page 32 – Figure 2-12 Glideslope Indicator; MARKER BEACON ANNUNCIATIONS; Figure 2-13 Marker Beacon Annunciations; VERTICAL SPEED INDICATOR; Figure 2-14 Vertical Speed Indicator; BAROMETRIC ALTITUDE MINIMUMS; Figure 2-15 Barometric Minimum Descent Altitude Settings
  • Page 33 – • When the aircraft passes through 100 feet of the; Figure 2-16 Barometric Minimum Descent Altitude; When the window is selected for display, but wind; Figure 2-17 Wind Data Window
  • Page 34 – HORIZONTAL SITUATION INDICATOR; Figure 2-18 Horizontal Situation Indicator; Turn Rate Indicator and Heading Trend Vector; Figure 2-20 Standard-Rate Turn Indication; Course Pointer; Figure 2-21 Course Pointer
  • Page 35 – The CDI scale automatically adjusts to the current; Flight Phase; depending on variables (see Figure; Figure 2-22 Phases of Flight/CDI Scaling
  • Page 36 – Figure 2-25 HSI with Bearing Information; Figure 2-28 DME Information Window; Navigation Source; CDI
  • Page 37 – The; Softkey is only displayed when
  • Page 39 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; DEFAULT ENGINE DISPLAY; Figure 3-1 Default Engine Display
  • Page 40 – FULL EIS DISPLAY; Fuel calculations do not use the aircraft; DEC FUEL; Figure 3-3 Full Engine Display
  • Page 41 – Figure 3-4 Full Engine Display; Leaning Assist (Normally Aspirated Engine Only); Adjust the
  • Page 43 – TRANSPONDER; The NAV/COM controls and frequency boxes share the
  • Page 44 – Figure 4-2 Frequency Fields
  • Page 45 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME; Figure 4-7 Radio Tuning Window; Figure 4-8 DME Selection Window
  • Page 46 – NRST; Auto-tuning on the MFD; Figure 4-10 Ground Mode; Code Number and; Figure 4-11 Standby Mode; Manual ON Mode; ON Mode
  • Page 47 – Altitude Mode is automatically selected when the air-; Figure 4-13 Altitude Mode; Reply Status; When the transponder sends replies to interrogations,; Figure 4-14 Reply Indication; Reply; Code Selection; The pre-programmed VFR Code is set at
  • Page 48 – If so configured, the Flight ID may be entered in the; Flight ID
  • Page 49 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 50 – COM RADIO SELECTION; Figure 5-2 Transceivers; SPLIT COM FUNCTION; Split COM performance is affected by the; MARKER BEACON RECEIVER; Figure 5-4 Marker Beacon Annunciators on the PFD
  • Page 51 – HI SENS; Figure 5-5 Marker Beacon; NAV RADIO AUDIO SELECTION; Table 5-1 ICS Isolation Modes; PILOT; Figure 5-7 ICS Isolation
  • Page 52 – INTERCOM SQUELCH CONTROL
  • Page 53 – SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FLIGHT; Refer to the pilot’s guide for the installed autopilot
  • Page 55 – SECTION 7 – NAVIGATION; SECTION 7: NAVIGATION; The majority of the following discussions pertain to; NAVIGATION MAP PAGE; The map display should only be; Select the MAP Page Group
  • Page 57 – Figure 7-6 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 59 – NAVIGATING AN EXAMPLE FLIGHT; The following discussion is an example of navigating a; If the loaded arrival procedure has
  • Page 61 – Figure 7-13 Begin Adding V4 to the Flight Plan; Figure 7-14 Entering V4 Entry Point; Figure 7-15 TOP Inserted into the Flight Plan
  • Page 62 – Figure 7-16 List of Available Airways for TOP
  • Page 63 – Figure 7-19 V4 is Loaded in the Flight Plan; Figure 7-20 Comfirm Active Leg; Figure 7-21 V4 Now Active Leg
  • Page 64 – Figure 7-22 Turn on to Active Leg
  • Page 65 – Figure 7-25 HYS to LAA Leg Active; Figure 7-26 Direct To OPSHN; Figure 7-27 Enter VNV Altitude
  • Page 66 – Figure 7-28 Enter VNV Offset Distance; Key. The altitude will now be displayed; PROC
  • Page 67 – Figure 7-30 Proceudures Window; Figure 7-31 List of Available Approaches; Figure 7-32 List of Available Transitions
  • Page 68 – Figure 7-33 Loaded Approach; Figure 7-34 Designate HABUK Altitude Constraint
  • Page 69 – Knob to select the altitude; Figure 7-35 Designate FALUR Altitude Constraint; Press the; Key to designate this altitude; Figure 7-36 Vertical Guidance is Active to the FAF; As the aircraft approaches OPSHN, it may
  • Page 70 – VNV PROF; Figure 7-37 Adjusting the Descent
  • Page 71 – Upon reaching TOD, a descent vertical speed is; Figure 7-40 VDI & RVSI Showing Correctly Established Descent; When the aircraft is one minute from the bottom; Offset Waypoint; The aircraft is approaching OPSHN. The upcoming; Figure 7-42 Turn to intercept OPSHN to FSHER Leg
  • Page 72 – After passing OPSHN, the next leg of the arrival; Figure 7-43 Tracking the OPSHN to FSHER Leg; The flight continues through the arrival procedure; Figure 7-44 Approaching PYNON
  • Page 73 – Figure 7-45 Approach Leg is Now Active; Figure 7-46 Activate Missed Approach; Figure 7-47 Descending Turn to the Initial Approach Fix (IAF)
  • Page 74 – After crossing FALUR the next waypoint is the; Figure 7-48 Descending to the FAF; After crossing CEGIX, the aircraft continues; Figure 7-49 Descending to the Missed Approach Point
  • Page 75 – ’) is not part of the published procedure.; Upon reaching the MAP, it is decided to execute; SUSP; Softkey on the PFD to resume automatic; Figure 7-50 Missed Approach Active
  • Page 76 – Figure 7-51 Establishing the Holding Pattern; AIRPORT INFORMATION; Figure 7-53 Airport Information Page; Select the Airport Information Page
  • Page 77 – Figure 7-54 Flight Plan Airport List
  • Page 78 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-57 Intersection Information Page
  • Page 79 – Figure 7-58 NDB Information Page; Select the NDB Information Page; Figure 7-59 VOR Information Page; Select the VOR Information Page
  • Page 80 – USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-60 Nearest Airports Page; Nearest Airport Information on the MFD
  • Page 81 – Figure 7-61 Nearest Airports Window; NEAREST INTERSECTIONS; Figure 7-62 Nearest Intersections Page; Select the Nearest Intersections Page
  • Page 82 – Figure 7-63 Nearest NDB Page; Select the Nearest NDB Page; Figure 7-64 Nearest VOR Page; Select the Nearest VOR Page
  • Page 83 – NEAREST USER WAYPOINT; Figure 7-65 Nearest User Waypoints Page; Select the Nearest User Waypoint Page; NEAREST FREQUENCIES; Figure 7-66 Nearest Frequencies Page; Select the Nearest Frequencies Page
  • Page 84 – NEAREST AIRSPACES; Figure 7-67 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an
  • Page 85 – SECTION 8 – FLIGHT PLANNING; The following discussions pertain to the Multi Function; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page
  • Page 86 – 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 87 – 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 88 – 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 89 – ENTER AN AIRWAY IN A FLIGHT; FPL; Figure 8-13 Airway Insertion Point; Figure 8-14 Load Airway Entry Point; Figure 8-15 Airway Entry Point Loaded; Figure 8-16 Display Waypoint Information Window; LD AIRWY
  • Page 90 – Figure 8-17 Select Desired Airway; Figure 8-18 Select Desired Exit Point; Figure 8-19 Airway Added to Flight Plan; LOAD A DEPARTURE
  • Page 91 – Figure 8-20 Store Flight Plan Confirmation
  • Page 92 – COPY A FLIGHT PLAN; Figure 8-22 Trip Planning Page; Starting WPT
  • Page 93 – The Page Mode must be set to MANUAL
  • Page 95 – 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 96 – Figure 9-4 Select Arrival Transition; Figure 9-5 Select Arrival Runway; Not all approaches in the database are approved for GPS; APPROACH
  • Page 97 – Figure 9-6 Selecting an Approach Procedure; Activate An Approach in the Active Flight Plan
  • Page 99 – SECTION 10 – HAZARD; SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 100 – 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 101 – Use of XM weather for hazardous; Figure 10-7 Navigation Map Page Displaying NEXRAD Weather; Figure 10-8 METAR and TAF Text Displayed on the
  • Page 102 – Figure 10-9 Weather Data Link Page
  • Page 104 – Figure 10-10 Weather Product Symbols; LOCK; Softkey on the AUX - XM; Weather Product Age; Weather Product
  • Page 105 – 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; Figure 10-11 Traffic Map Page; Displaying Traffic on the Navigation Map; “Traffic Not Available” will be heard whenever TIS
  • Page 106 – TRAFFIC ADVISORY; Refer to the SkyWatch pilot’s guide for a detailed; Figure 10-12 Traffic Map Page
  • Page 107 – Figure 10-13 TAS Traffic on Navigation Map; Traffic Advisory; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Color
  • Page 108 – Figure 10-15 Obstacle Symbols; Displaying Terrain on the TAWS Page
  • Page 109 – Black
  • Page 110 – Figure 10-18 TAWS Page Menu; TAWS Inhibit; TAWS System
  • Page 111 – Phase of Flight; Enroute; Figure 10-19 PDA Alerting; Negative Climb Rate After Takeoff; Don’t Sink
  • Page 112 – Figure 10-21 Negative Climb Rate; “Five-Hundred” Aural Alert; Potential Impact Points; Figure 10-22 TAWS Symbols; Displaying Terrain and Obstacles on the; With the Navigation Map displayed, press the; TERRAIN; Softkey. Terrain and obstacle
  • Page 113 – Alert Type
  • Page 114 – The following system status annunciations may also be; Alert Annunciations; Figure 10-24 Alert Annunciation on the TAWS Page; Alert Annuciation; Figure 10-25 Alert Annunciation on the PFD
  • Page 115 – SECTION 11 – ABNORMAL; SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; ABNORMAL COM OPERATION; When a COM tuning failure is detected by the system,
  • Page 116 – UNUSUAL ATTITUDES; Figure 11-2 Extreme Pitch Indication; STORMSCOPE OPERATION WITH; Figure 11-3 Loss of Hazard Functions with Loss of GPS Position
  • Page 117 – Figure 11-4 Dead Reckoning Indications; Symbolic Aircraft
  • Page 119 – SECTION 12 – ANNUNCIATIONS
  • Page 120 – ALERT LEVEL DEFINITIONS
  • Page 121 – AIRCRAFT ALERTS; information regarding pilot responses.; WARNING Alerts
  • Page 124 – Figure 12-5 G1000 System Failure Annunciations; System Annunciation
  • Page 126 – Message Advisory Alerts; Alerts Window Message; MFD & PFD Message Advisories
  • Page 136 – Message; – Stormscope has; FAILED PATH; MAG VAR WARN; – Large magnetic
  • Page 137 – INDEX; Signal augmentation 5-3
  • Page 138 – Load the nearest ARTCC frequency
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Integrated Flight Deck

Cockpit Reference Guide

Piper

PA32

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Summary

Page 3 - Garmin G1000 Cockpit Reference Guide for the Piper PA32

Garmin G1000 Cockpit Reference Guide for the Piper PA32 Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0648.02 or later for the Piper PA32. Some differences in operation may be observed when comparing the infor...

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the Piper PA32 RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00416-00 Rev A Rev B Initial release. Revised for system software version 0426.01 190-00416-01 Rev A Added GDU 7.0 software parameters, WAAS, VNAV, electronic charts, TAWS, and full EIS di...

Page 8 - Blank Page

Garmin G1000 Cockpit Reference Guide for the Piper PA32 RR-2 RECORD OF REVISIONS Blank Page

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