- •Section 1 System Overview
- •1.1 System Description
- •1.2 Line Replaceable Units (LRU)
- •1.3 G1000 Controls
- •PFD/MFD Controls
- •Audio Panel Controls
- •1.4 Secure Digital (SD) Cards
- •1.5 System Power-up
- •1.6 System Operation
- •Normal Display Operation
- •Reversionary Display Operation
- •AHRS Operation
- •G1000 System Annunciations
- •Softkey Function
- •GPS Receiver Operation
- •1.7 Accessing G1000 Functionality
- •Menus
- •MFD Page Groups
- •MFD System Pages
- •Electronic Checklists (Optional)
- •1.8 Display Backlighting
- •Automatic Adjustment
- •Manual Adjustment
- •Section 2 flight Instruments
- •2.1 Flight Instruments
- •Airspeed Indicator
- •Attitude Indicator
- •Altimeter
- •Vertical Speed Indicator (VSI)
- •Vertical Deviation, Glideslope, & Glidepath Indicators
- •Horizontal Situation Indicator (HSI)
- •Course Deviation Indicator (CDI)
- •2.2 Supplemental Flight Data
- •Generic Timer
- •Outside Air Temperature
- •Wind Data
- •System Time
- •Vertical Navigation (VNV) Indications
- •2.3 PFD Annunciations and Alerting Functions
- •System Alerting
- •Traffic Annunciation
- •TAWS Annunciations
- •Low Altitude Annunciation
- •Altitude Alerting
- •Minimum Descent Altitude/Decision Height Alerting
- •Marker Beacon Annunciations
- •2.4 Abnormal Operations
- •Abnormal GPS Conditions
- •Unusual Attitudes
- •Section 3 Engine Indication System (EIS)
- •3.1 Engine Display
- •3.2 Lean Display
- •3.3 System Display
- •Section 4 audio panel and CNS
- •4.1 Overview
- •PFD/MFD Controls and Frequency Display
- •Audio Panel Controls
- •4.2 COM Operation
- •COM Transceiver Selection and Activation
- •COM Transceiver Manual Tuning
- •Quick-Tuning and Activating 121.500 MHz
- •Auto-tuning the COM Frequency
- •Frequency Spacing
- •Automatic Squelch
- •Volume
- •4.3 NAV Operation
- •NAV Radio Selection and Activation
- •NAV Receiver Manual Tuning
- •Auto-tuning the NAV Frequency
- •Marker Beacon Receiver
- •DME Tuning (Optional)
- •4.4 GTX 33 Mode S Transponder
- •Transponder Controls
- •Transponder Mode Selection
- •Entering a Transponder Code
- •IDENT Function
- •Flight ID Reporting
- •4.5 Additional Audio Panel Functions
- •Power-Up
- •Mono/Stereo Headsets
- •Speaker
- •Intercom
- •Clearance Recorder and Player
- •Entertainment Inputs
- •4.6 Audio Panel Preflight Procedure
- •4.7 Abnormal Operation
- •Stuck Microphone
- •COM Tuning Failure
- •Audio Panel Fail-Safe Operation
- •Reversionary Mode
- •Section 5 GPS Navigation
- •5.1 Introduction
- •5.2 Navigation Map (MFD)
- •Navigation Map Page
- •5.3 PFD Inset Map and Windows
- •Inset Map
- •PFD Windows
- •5.4 Direct-to-Navigation (MFD)
- •Selecting a Direct-to Waypoint
- •Clearing Vertical Constraints
- •Specifying a Course to a Waypoint
- •Canceling Direct-to Navigation
- •Direct-to Navigation Shortcuts
- •5.5 Direct-to-Navigation (PFD)
- •5.6 Airport Information (MFD)
- •Duplicate Waypoints
- •Additional Airport Runway Information
- •5.7 Intersection Information (MFD)
- •5.8 NDB Information (MFD)
- •5.9 VOR Information (MFD)
- •5.10 User Waypoint Information (MFD)
- •5.11 Nearest Airports (MFD)
- •5.12 Nearest Intersections (MFD)
- •5.13 Nearest NDB (MFD)
- •5.14 Nearest VOR (MFD)
- •5.15 Nearest User Waypoint (MFD)
- •5.16 Nearest Airspaces
- •5.17 Nearest Airports (PFD)
- •5.18 Flight Planning (MFD)
- •Airways/Jetways
- •Display of Airways on the Flight Plan Page
- •Vertical Navigation (VNV)
- •Navigating an Example Flight Plan
- •Parallel Track (PTK)
- •5.19 Flight Planning (PFD)
- •Operations
- •5.20 Procedures (MFD)
- •Leg Types Supported by the G1000
- •5.21 Procedures (PFD)
- •Operations
- •5.22 ABNORMAL OPERATION
- •Dead Reckoning
- •Section 6 Hazard Avoidance
- •6.1 XM Satellite Weather (Service Optional)
- •Activating XM Satellite Services
- •Using XM SATELLITE Weather Products
- •Weather Softkeys on the Weather Data Link Page
- •Setting Up the Weather Data Link Page
- •XM Satellite Weather on the Navigation Map
- •6.2 WX-500 Stormscope (Optional)
- •Setting Up Stormscope on the Navigation Map
- •Selecting the Stormscope Page
- •6.3 Terrain Proximity
- •Requirements
- •GPS Position and GPS-MSL Altitude
- •Displaying Terrain Proximity Data
- •Terrain Proximity Symbols
- •Terrain Proximity Page
- •Navigation Map Page
- •6.4 TAWS (Optional)
- •Requirements
- •TAWS Alerting
- •Using TAWS
- •TAWS Symbols
- •TAWS Alerts
- •6.5 Traffic
- •Traffic Information Service (TIS)
- •Honeywell KTA 870 TAS System (Optional)
- •ADS-B Traffic (Optional)
- •Section 7 Automatic Flight Control System
- •7.1 AFCS Controls
- •7.2 Flight Director Operation
- •Command Bars
- •Activating the Flight Director
- •7.3 Flight Director Modes
- •Pitch Modes
- •Roll Modes
- •7.4 Autopilot Operation
- •Engaging the Autopilot
- •Control Wheel Steering
- •Disengaging the Autopilot
- •7.5 Example Procedures
- •Departure
- •Intercepting a VOR Radial
- •Flying a Flight Plan/GPS Course
- •Descent
- •Approach
- •Go Around/Missed Approach
- •7.6 AFCS Annunciations and Alerts
- •AFCS Status Alerts
- •Overspeed Protection
- •Section 8 Additional Features
- •8.1 SafeTaxi
- •SafeTaxi Cycle Number and Revision
- •8.2 ChartView
- •ChartView Softkeys
- •Terminal Procedures Charts
- •Chart Options
- •Day/Night View
- •ChartView Cycle Number and Expiration Date
- •8.3 FliteCharts
- •FliteCharts Softkeys
- •Terminal Procedures Charts
- •Chart Options
- •Day/Night View
- •FliteCharts Cycle Number and Expiration Date
- •8.4 XM Radio Entertainment (Optional)
- •XM Satellite Radio Service
- •XM Service Activation
- •Using XM Radio
- •Automatic Audio Muting
- •8.5 Abnormal Operation
- •Annunciations and Alerts
- •Alert Level Definitions
- •NAV III Aircraft Alerts
- •CO Guardian Messages
- •G1000 System Annunciations
- •Other G1000 Aural Alerts
- •G1000 System Message Advisories
- •AFCS Alerts
- •TAWS ALERTS
- •TAWS System Status Annunciations
- •SD Card Use
- •Jeppesen Databases
- •Garmin Databases
- •Glossary
- •Frequently Asked Questions
- •General TIS Information
- •Introduction
- •TIS vs. TAS/TCAS
- •TIS Limitations
- •Map Symbols
- •Index
APPENDIX A
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
STRMSCP FAIL – Stormscope has |
Stormscope has failed. The G1000 system should be serviced. |
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failed. |
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FAILED PATH – A data path has failed. |
A data path connected to the GDU or the GIA 63/W has failed. |
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MAG VAR WARN – Large magnetic |
The GDU’s internal model cannot determine the exact magnetic variance for |
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variance. Verify all course angles. |
geographic locations near the magnetic poles. Displayed magnetic course angles may |
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differ from the actual magnetic heading by more than 2°. |
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SCHEDULER [#] – <message>. |
Message criteria entered by the user. |
AFCS ALERTS
System Status Field
Figure A-6 AFCS System Status Field
The following alert annunciations appear in the AFCS System Status field on the PFD.
Condition |
Annunciation |
Description |
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Pitch Failure |
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Pitch axis control failure. AP is inoperative. |
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Roll Failure |
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Roll axis control failure. AP is inoperative. |
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MET Switch Stuck, or |
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If annunciated when AP is engaged, take control of the aircraft and disengage the autopilot. |
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Pitch Trim Axis Control |
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If annunciated when AP is not engaged, move each half of the MET switch separately to |
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Failure |
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check if a stuck switch is causing the annunciation. |
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System Failure |
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AP and MET are unavailable. FD may still be available. |
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Elevator Mistrim Up |
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A condition has developed causing the pitch servo to provide a sustained force. Be prepared |
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to apply nose up control wheel force upon autopilot disconnect. |
Elevator Mistrim |
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A condition has developed causing the pitch servo to provide a sustained force. Be prepared |
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Down |
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to apply nose down control wheel force upon autopilot disconnect. |
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Aileron Mistrim Left |
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A condition has developed causing the roll servo to provide a sustained left force. Ensure |
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the slip/skid indicator is centered and observe any maximum fuel imbalance limits. |
Aileron Mistrim Right |
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A condition has developed causing the roll servo to provide a sustained right force. Ensure |
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the slip/skid indicator is centered and observe any maximum fuel imbalance limits. |
Preflight Test |
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Performing preflight system test. Upon completion of the test, the aural alert will be heard. |
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Preflight system test has failed. |
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NOTE: Do not press the AP DISC switch during servo power-up and preflight system tests as this may cause the preflight system test to fail or never to start (if servos fail their power-up tests). Power must be cycled to the servos to remedy the situation.
A-16 |
Garmin G1000 Pilot’s Guide for Cessna Nav III |
190-00498-02 Rev.A |
APPENDIX A
TAWS ALERTS
Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
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PFD/MFD |
MFD Map Page |
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Alert Type |
TAWS Page |
Aural Message |
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Pop-Up Alert |
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Annunciation |
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Excessive Descent RateWarning (EDR) |
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“Pull Up” |
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Reduced RequiredTerrain Clearance |
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“Terrain,Terrain; Pull Up, Pull Up” |
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Warning (RTC) |
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or |
or |
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“TerrainAhead, Pull Up;TerrainAhead, Pull Up” |
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ImminentTerrain ImpactWarning (ITI) |
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TerrainAhead, Pull Up;TerrainAhead, Pull Up” |
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or |
or |
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“Terrain,Terrain; Pull Up, Pull Up” |
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Reduced Required Obstacle Clearance |
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“Obstacle, Obstacle; Pull Up, Pull Up” |
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Warning (ROC) |
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or |
or |
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“ObstacleAhead, Pull Up; ObstacleAhead, Pull Up” |
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Imminent Obstacle ImpactWarning |
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“ObstacleAhead, Pull Up; ObstacleAhead, Pull Up” |
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(IOI) |
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or |
or |
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“Obstacle, Obstacle; Pull Up, Pull Up” |
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Reduced RequiredTerrain Clearance |
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“Caution,Terrain; Caution,Terrain” |
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Caution (RTC) |
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or |
or |
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“TerrainAhead;TerrainAhead” |
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ImminentTerrain Impact Caution (ITI) |
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“TerrainAhead;TerrainAhead” |
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or |
or |
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“Caution,Terrain; Caution,Terrain” |
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Reduced Required Obstacle Clearance |
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“Caution, Obstacle; Caution, Obstacle” |
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Caution (ROC) |
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or |
or |
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“ObstacleAhead; ObstacleAhead” |
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Imminent Obstacle Impact Caution |
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“ObstacleAhead; ObstacleAhead” |
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(IOI) |
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or |
or |
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“Caution, Obstacle; Caution, Obstacle” |
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Premature DescentAlert Caution (PDA) |
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“Too Low,Terrain” |
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Altitude Callout “500” |
None |
None |
“Five-Hundred” |
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Excessive Descent Rate Caution (EDR) |
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“Sink Rate” |
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Negative Climb Rate Caution (NCR) |
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“Don’t Sink” |
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or |
or |
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“Too Low,Terrain” |
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190-00498-02 Rev.A |
Garmin G1000 Pilot’s Guide for Cessna Nav III |
A-17 |
APPENDIX A
TAWS SYSTEM STATUS ANNUNCIATIONS
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PFD/MFD |
MFD |
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Alert Type |
TAWS Page |
Aural Message |
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Pop-Up Alert |
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Annunciation |
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TAWS System Test Fail |
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None |
“TAWS System Failure” |
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TAWS Alerting is disabled |
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None |
None |
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No GPS position or excessively |
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None |
“TAWS Not Available” |
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degraded GPS signal |
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“TAWS Available” will be heard when sufficient |
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GPS signal is re-established. |
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System Test in progress |
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None |
None |
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System Test pass |
None |
None |
“TAWS System Test OK” |
A-18 |
Garmin G1000 Pilot’s Guide for Cessna Nav III |
190-00498-02 Rev.A |