apply nose down control wheel force upon autopilot disconnect. Preflight system test has failed.

Transcription

1 13.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 13-5 AFCS System Status Annunciation Condition Annunciation Description Pitch Failure Pitch axis control failure. AP is inoperative. Roll Failure MET Switch Stuck, Pitch Trim Axis Control Failure System Failure Elevat Mistrim Up Elevat Mistrim Down Aileron Mistrim Left Aileron Mistrim Right Preflight Test Roll axis control failure. AP is inoperative. If annunciated when AP is engaged, take control of the aircraft and disengage the autopilot. If annunciated when AP is not engaged, move each half of the MET switch separately to check if a stuck switch is causing the annunciation. AP and MET are unavailable. FD may still be available. A condition has developed causing the pitch servo to provide a sustained fce. Be prepared to apply nose up control wheel fce upon autopilot disconnect. A condition has developed causing the pitch servo to provide a sustained fce. Be prepared to apply nose down control wheel fce upon autopilot disconnect. A condition has developed causing the roll servo to provide a sustained left fce. Ensure the slip/ skid indicat is centered and observe any maximum fuel imbalance limits. A condition has developed causing the roll servo to provide a sustained right fce. Ensure the slip/skid indicat is centered and observe any maximum fuel imbalance limits. Perfming preflight system test. Upon completion of the test, the aural alert is heard. Preflight system test has failed Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

2 13.5 TERRAIN-SVS ALERTS The following table shows the possible Terrain-SVS alert types with cresponding annunciations and aural messages. Alert Type PFD/MFD Alert Annunciation MFD Pop-Up Alert Aural Reduced Required Terrain Clearance Warning (RTC) Warning; Terrain, Terrain Imminent Terrain Impact Warning (ITI) Warning; Terrain, Terrain Reduced Required Obstacle Clearance Warning (ROC) Warning; Obstacle, Obstacle Imminent Obstacle Impact Warning (IOI) Warning; Obstacle, Obstacle Reduced Required Terrain Clearance Caution (RTC) Caution; Terrain, Terrain Imminent Terrain Impact Caution (ITI) Caution; Terrain, Terrain Reduced Required Obstacle Clearance Caution (ROC) Caution; Obstacle, Obstacle Imminent Obstacle Impact Caution (IOI) Caution; Obstacle, Obstacle The following system status annunciations may also be issued. Alert Type PFD/MFD Alert Annunciation TERRAIN-SVS Page Annunciation Aural System Test in Progress TERRAIN TEST None System Test Pass None None Terrain System Test OK Terrain Alerting is disabled None None MFD Terrain Obstacle database unavailable invalid. Terrain-SVS operating with PFD Terrain Obstacle databases None TERRAIN DATABASE FAILURE None Terrain System Test Fail TERRAIN FAIL Terrain System Failure Terrain Obstacle database unavailable invalid, invalid software configuration, system audio fault TERRAIN FAIL Terrain System Failure Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-5

3 Alert Type PFD/MFD Alert Annunciation TERRAIN-SVS Page Annunciation Aural No GPS position NO GPS POSITION Terrain System Not Available Excessively degraded GPS signal, Out of database coverage area None Terrain System Not Available Sufficient GPS signal received after loss None None Terrain System Available 13.6 TAWS ALERTS The following table shows the possible TAWS alert types with cresponding annunciations and aural messages. Alert Type Excessive Descent Rate Warning (EDR) PFD/MFD TAWS-B Page Annunciation MFD Pop-Up Alert Aural Pull Up Reduced Required Terrain Clearance Warning (RTC) Imminent Terrain Impact Warning (ITI) Reduced Required Obstacle Clearance Warning (ROC) Imminent Obstacle Impact Warning (IOI) Reduced Required Terrain Clearance Caution (RTC) Imminent Terrain Impact Caution (ITI) Reduced Required Obstacle Clearance Caution (ROC) Imminent Obstacle Impact Caution (IOI) Terrain, Terrain; Pull Up, Pull Up Terrain Ahead, Pull Up; Terrain Ahead, Pull Up Terrain Ahead, Pull Up; Terrain Ahead, Pull Up Terrain, Terrain; Pull Up, Pull Up Obstacle, Obstacle; Pull Up, Pull Up Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up Obstacle, Obstacle; Pull Up, Pull Up Caution, Terrain; Caution, Terrain Terrain Ahead; Terrain Ahead Terrain Ahead; Terrain Ahead Caution, Terrain; Caution, Terrain Caution, Obstacle; Caution, Obstacle Obstacle Ahead; Obstacle Ahead Obstacle Ahead; Obstacle Ahead Caution, Obstacle; Caution, Obstacle 13-6 Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

4 Alert Type PFD/MFD TAWS-B Page Annunciation MFD Pop-Up Alert Aural Premature Descent Alert Caution (PDA) Too Low, Terrain Altitude Callout 500 None None Five-Hundred Excessive Descent Rate Caution (EDR) Sink Rate Negative Climb Rate Caution (NCR) Don t Sink Too Low, Terrain TAWS SYSTEM STATUS ANNUNCIATIONS Alert Type PFD/MFD Alert Annunciation TERRAIN-SVS Page Annunciation Aural System Test in Progress TAWS TEST None System Test Pass None None TAWS System Test OK MFD Terrain Obstacle database unavailable invalid. TAWS operating with PFD Terrain Obstacle databases None TERRAIN DATABASE FAILURE None TAWS-B System Test Fail TAWS FAIL TAWS System Failure Terrain Obstacle database unavailable invalid, invalid software configuration, system audio fault TAWS FAIL TAWS System Failure No GPS position NO GPS POSITION TAWS Not Available Excessively degraded GPS signal, Out of database coverage area None TAWS Not Available Sufficient GPS signal received after loss None None TAWS Available Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-7

5 13.7 OTHER G1000 AURAL ALERTS Aural Alert Minimums, minimums Vertical track Traffic Traffic not available Traffic, Traffic One o clock through Twelve o clock No Bearing High, Low, Same Altitude (if within 200 feet of own altitude), Altitude not available Less than one mile, One Mile through Ten Miles, Me than ten miles Description The aircraft has descended below the preset barometric minimum descent altitude. The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled. The Traffic Infmation Service (TIS) ADS-B traffic system has issued a Traffic Advisy alert The aircraft is outside the Traffic Infmation Service (TIS) ADS-B coverage area. Played when a Traffic Advisy (TA) is issued (TAS system). Played to indicate bearing of traffic from own aircraft (GTS 800 only). Played to indicate altitude of traffic relative to own aircraft (GTS 800 only). Played to indicate distance of traffic from own aircraft (GTS 800 only) Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

6 13.8 G1000 SYSTEM ANNUNCIATIONS When an LRU an LRU function fails, a large red X is typically displayed on areas associated with the failed data. Refer to the POH f additional infmation regarding pilot responses to these annunciations. NOTE: Upon power-up of the G1000 system, certain boxes remain invalid as G1000 equipment begins to initialize. All boxes should be operational within one minute of power-up. Should any box continue to remain flagged, the G1000 system should be serviced by a Garmin-authized repair facility. System Annunciation Comment Attitude and Heading Reference System is aligning. Display system is not receiving attitude infmation from the AHRS. Indicates a configuration module failure. This annunciation is only seen when the autopilot is engaged. The annunciation indicates an AHRS monit has detected an abnmal flight parameter, possibly caused by strong turbulence. In this case, the situation should crect itself within a few seconds. If there is an actual failure, a red X soon appears over the Attitude Indicat. Display system is not receiving airspeed input from air data computer Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-9

7 System Annunciation Comment Display is not receiving altitude input from the air data computer. Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. Display is not receiving valid transponder infmation. Different versions of GDU software are installed in the PFD and MFD. This can also indicate different versions of navigation databases are installed in the PFD and MFD. In some circumstances, a cross-talk err between the PFD and MFD can cause this annunciation. LOI Indicates Loss of Integrity of GPS infmation. GPS infmation is either not present is invalid f navigation use. DR may also be seen indicating that GPS is in Dead Reckoning Mode. Note that AHRS utilizes GPS inputs during nmal operation. AHRS operation may be degraded if GPS signals are not present (see AFMS). Other Various Red X Indications A red X through any other display field, such as engine instrumentation fields, indicates that the field is not receiving valid data Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

8

9

10 System Components Two Control Display Units Audio Panel Attitude and Heading Reference System Air Data Computer Engine/Airframe Unit Two Integrated Avionics Units Data Link Mode S Transponder Magnetometer 2010 Cessna Aircraft Company. Version 10a

11 G1000 Components Two Control Display Units = GDU Marker/Audio Panel = GMA Attitude and Heading Reference System = GRS Air Data Computer = GDC Engine/Airframe Unit = GEA Two Integrated Avionics Units = GIA Data Link = GDL Mode S Transponder X = GTX Magnetometer Unit = GMU 2010 Cessna Aircraft Company. Version 10a

12 G1000 System Advisies GIA 1 CONFIG - GIA 1 config err. Config service req d. GMA 1 FAIL - GMA 1 is inoperative Cessna Aircraft Company. Version 10a

13 Auxiliary System Status 2010 Cessna Aircraft Company. Version 10a

14 Control Display Units Primary Flight Display (PFD) Multi-Function Display (MFD) GDU 1040/1044B Garmin Control Display Unit Best resolution on the market 1044B contains AFCS mode select buttons Reversionary capabilities 2010 Cessna Aircraft Company. Version 10a

15 Attitude and Heading Reference System-AHRS GRS 77 Source f: Attitude Heading Rate of Turn Slip/Skid Solid State Me reliable than conventional vacuum gyros On-the-Run Initialization Tail Cone Avionics Bay 2010 Cessna Aircraft Company. Version 10a

16 Air Data Computer - ADC GDC 74A Source f: Altitude Indicated Airspeed Vertical Speed Outside Air Temperature True Airspeed Wind Vect Located: Behind Instrument Panel (182/206) Tailcone Avionics Bay(172) 2010 Cessna Aircraft Company. Version 10a

17 Engine/Airframe Unit GEA 71 Receives data from airframe and engine systems Presents the infmation on the Engine Indication System (EIS) Provides System Integrity Moniting Behind Instrument Panel 2010 Cessna Aircraft Company. Version 10a

18 Integrated Avionics Unit GIA 63W WAAS-Enabled Similar to a Garmin 530A without the display interface Dual GPS, NAV, and COM Radios Redundancy Reliability 16 watts 8.33 khz spacing Tail Cone Avionics Bay 2010 Cessna Aircraft Company. Version 10a

19 Garmin Data Link GDL 69A XM Satellite Radio Receiver Near, Real-time Weather Digital Audio Entertainment Subscription Service 2010 Cessna Aircraft Company. Version 10a

20 Transponder GTX 33 Mode S Transponder Automatic activation feature at approximately 30 knots Traffic Infmation Service -TIS Tail Cone Avionics Bay 2010 Cessna Aircraft Company. Version 10a

21 Magnetometer GMU 44 3 Axis Magnetic Sens Replaces traditional Flux Valve Located in Left Wing 2010 Cessna Aircraft Company. Version 10a

22 A red X may be the result of an LRU an LRU function failure. The Figure 13-6 illustrates all possible flags and the responsible LRUs. GIA 63/63W Integrated Avionics Units GIA 63/63W Integrated Avionics Units GDC 74A Air Data Computer GEA 71 Engine Airframe Unit Or GIA 63/63W Integrated Avionics Unit Database Mismatch in PFD and MFD GRS 77 AHRS Or GMU 44 Magnetometer GIA 63/63W Integrated Avionics Units GDC 74A Air Data Computer Figure 13-6 G1000 System Failure Annunciations GTX 33 Transponder Or GIA 63/63W Integrated Avionics Units Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-11

23 13.9 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisies. Certain messages are issued due to an LRU an LRU function failure. Such messages are nmally accompanied by a cresponding red X annunciation as shown previously in the G1000 System Annunciation section. NOTE: This section provides infmation regarding G1000 message advisies that may be displayed by the system. Knowledge of the aircraft, systems, flight conditions, and other existing operational priities must be considered when responding to a message. Always use sound pilot judgment. The Cessna aircraft Pilot s Operating Handbook (POH) takes precedence over any conflicting guidance found in this section. MFD & PFD Advisies DATA LOST Pilot sted data was lost. Recheck settings. XTALK ERROR A flight display crosstalk err has occurred. PFD1 SERVICE PFD1 needs service. Return unit f repair. MFD1 SERVICE MFD1 needs service. Return unit f repair. MANIFEST PFD1 software mismatch, communication halted. MANIFEST MFD1 software mismatch, communication halted. PFD1 CONFIG PFD1 config err. Config service req d. MFD1 CONFIG MFD1 config err. Config service req d. SW MISMATCH GDU software version mismatch. Xtalk is off. PFD1 COOLING PFD1 has po cooling. Reducing power usage. MFD1 COOLING MFD1 has po cooling. Reducing power usage. The pilot profile data was lost. System reverts to default pilot profile and settings. The pilot may reconfigure the MFD & PFDs with preferred settings, if desired. The MFD and PFD are not communicating with each other. The system should be serviced. The PFD and/ MFD self-test has detected a problem. The system should be serviced. The PFD and/ MFD has increct software installed. The system should be serviced. The PFD configuration settings do not match backup configuration memy. The system should be serviced. The MFD configuration settings do not match backup configuration memy. The system should be serviced. The MFD and PFD have different software versions installed. The system should be serviced. The PFD and/ MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

24 MFD & PFD Advisies (Cont.) PFD1 KEYSTK PFD1 [key name] Key is stuck. MFD1 KEYSTK MFD [key name] Key is stuck. CNFG MODULE PFD1 configuration module is inoperative. PFD1 VOLTAGE PFD1 has low voltage. Reducing power usage MFD1 VOLTAGE MFD1 has low voltage. Reducing power usage A key is stuck on the PFD and/ MFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. The PFD1 configuration module backup memy has failed. The system should be serviced. The PFD1 voltage is low. The system should be serviced. The MFD voltage is low. The system should be serviced. Database Advisies MFD1 DB ERR MFD1 navigation database err exists. PFD1 DB ERR PFD1 navigation database err exists. MFD1 DB ERR MFD1 basemap database err exists. PFD1 DB ERR PFD1 basemap database err exists. MFD1 DB ERR MFD1 terrain database err exists. PFD1 DB ERR PFD1 terrain database err exists. MFD1 DB ERR MFD1 terrain database missing. PFD1 DB ERR PFD1 terrain database missing. The MFD and/ PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. The MFD and/ PFD detected a failure in the basemap database. The MFD and/ PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, the system should be serviced. The terrain database is present on another LRU, but is missing on the specified LRU Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-13

25 Database Advisies (Cont.) MFD1 DB ERR MFD1 obstacle database err exists. PFD1 DB ERR PFD1 obstacle database err exists. MFD1 DB ERR MFD1 obstacle database missing. PFD1 DB ERR PFD1 obstacle database missing. MFD1 DB ERR MFD1 airpt terrain database err exists. PFD1 DB ERR PFD1 airpt terrain database err exists. MFD1 DB ERR MFD1 airpt terrain database missing. PFD1 DB ERR PFD1 airpt terrain database missing. MFD1 DB ERR MFD1 Safe Taxi database err exists. PFD1 DB ERR PFD1 Safe Taxi database err exists. MFD1 DB ERR MFD1 Chartview database err exists. MFD1 DB ERR MFD1 FliteCharts database err exists. MFD1 DB ERR MFD1 Airpt Directy database err exists. The MFD and/ PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The obstacle database is present on another LRU, but is missing on the specified LRU. The MFD and/ PFD detected a failure in the airpt terrain database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The airpt terrain database is present on another LRU, but is missing on the specified LRU. The MFD and/ PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The MFD detected a failure in the ChartView database (optional feature). Ensure the data card is properly inserted. Replace data card. If problem persists, system should be serviced. The MFD detected a failure in the FliteCharts database (optional feature). Ensure the data card is properly inserted. Replace data card. If problem persists, system should be serviced. The MFD detected a failure in the Airpt Directy database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

26 Database Advisies (Cont.) DB MISMATCH Navigation database mismatch. Xtalk is off. DB MISMATCH Terrain database mismatch. DB MISMATCH Obstacle database mismatch. DB MISMATCH Airpt Terrain database mismatch. DB MISMATCH Standby Navigation database mismatch. NAV DB UPDATED Active navigation database updated. TERRAIN DSP [PFD1 MFD1] Terrain awareness display unavailable. The PFD and MFD have different navigation database versions regions installed. Crossfill is off. Check the AUX-SYSTEM STATUS Page to determine versions regions. Also, check the AUX-SYSTEM STATUS Page f a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. The PFD and MFD have different terrain database versions regions installed. Check the AUX-SYSTEM STATUS Page to determine versions regions. Also, check the AUX-SYSTEM STATUS Page f a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. The PFD and MFD have different obstacle database versions regions installed. Check the AUX-SYSTEM STATUS Page to determine versions regions. Also, check the AUX-SYSTEM STATUS Page f a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. The PFD and MFD have different airpt terrain database versions regions installed. Check the AUX-SYSTEM STATUS Page to determine versions regions. Also, check the AUX-SYSTEM STATUS Page f a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. The PFD and MFD have different standby navigation database versions regions installed. Check the AUX-SYSTEM STATUS Page to determine versions regions. Also, check the AUX-SYSTEM STATUS Page f a database synchronization function not completed. After synchronization is complete, power must be turned off, then on. System has updated the active navigation database from the standby navigation database. One of the terrain, airpt terrain, obstacle databases required f TAWS in the specified PFD MFD is missing invalid Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-15

27 GMA 1347 Advisies GMA1 FAIL GMA1 is inoperative. GMA1 CONFIG GMA1 config err. Config service req d. MANIFEST GMA1 software mismatch, communication halted. GMA1 SERVICE GMA1 needs service. Return unit f repair. The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced. The audio panel configuration settings do not match backup configuration memy. The system should be serviced. The audio panel has increct software installed. The system should be serviced. The audio panel self-test has detected a problem in the unit. Certain audio functions may still be available, and the audio panel may still be usable. The system should be serviced when possible. GIA 63 Advisies GIA1 CONFIG GIA1 config err. Config service req d. GIA2 CONFIG GIA2 config err. Config service req d. GIA1 CONFIG GIA1 audio config err. Config service req d. GIA2 CONFIG GIA2 audio config err. Config service req d. GIA1 COOLING GIA1 temperature too low. GIA2 COOLING GIA2 temperature too low. GIA1 COOLING GIA1 over temperature. GIA2 COOLING GIA2 over temperature. GIA1 SERVICE GIA1 needs service. Return the unit f repair. GIA2 SERVICE GIA2 needs service. Return the unit f repair. The GIA1 and/ GIA2 configuration settings do not match backup configuration memy. The G1000 system should be serviced. The GIA1 and/ GIA2 have an err in the audio configuration. The G1000 system should be serviced. The GIA1 and/ GIA2 temperature is too low to operate crectly. Allow units to warm up to operating temperature. The GIA1 and/ GIA2 temperature is too high. If problem persists, the G1000 system should be serviced. The GIA1 and/ GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

28 GIA 63 Advisies (Cont.) MANIFEST GIA1 software mismatch, communication halted. MANIFEST GIA2 software mismatch, communication halted. COM1 TEMP COM1 over temp. Reducing transmitter power. COM2 TEMP COM2 over temp. Reducing transmitter power. COM1 SERVICE COM1 needs service. Return unit f repair. COM2 SERVICE COM2 needs service. Return unit f repair. COM1 PTT COM1 push-to-talk key is stuck. COM2 PTT COM2 push-to-talk key is stuck. COM1 RMT XFR COM1 remote transfer key is stuck. COM2 RMT XFR COM2 remote transfer key is stuck. RAIM UNAVAIL RAIM is not available from FAF to MAP waypoints. LOI GPS integrity lost. Crosscheck with other NAVS. GPS NAV LOST Loss of GPS navigation. Insufficient satellites. GPS NAV LOST Loss of GPS navigation. Position err. GPS NAV LOST Loss of GPS navigation. GPS fail. The GIA1 and/ GIA 2 has increct software installed. The G1000 system should be serviced. The system has detected an over temperature condition in COM1 and/ COM2. The transmitter is operating at reduced power. If the problem persists, the G1000 system should be serviced. The system has detected a failure in COM1 and/ COM2. COM1 and/ COM2 may still be usable. The G1000 system should be serviced when possible. The COM1 and/ COM2 external push-to-talk switch is stuck in the enable ( pressed ) position. Press the PTT switch again to cycle its operation. If the problem persists, the G1000 system should be serviced. The COM1 and/ COM2 transfer switch is stuck in the enabled ( pressed ) position. Press the transfer switch again to cycle its operation. If the problem persists, the G1000 system should be serviced. GPS satellite coverage is insufficient to perfm Receiver Autonomous Integrity Moniting (RAIM) from the FAF to the MAP waypoints. Loss of GPS integrity moniting. Loss of GPS navigation due to insufficient satellites. Loss of GPS navigation due to position err. Loss of GPS navigation due to GPS failure Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-17

29 GIA 63 Advisies (Cont.) ABORT APR Loss of GPS navigation. Abt approach. TRUE APR True nth approach. Change hdg reference to TRUE. GPS1 FAIL GPS1 is inoperative. GPS2 FAIL GPS2 is inoperative. GPS1 SERVICE GPS1 needs service. Return unit f repair. GPS2 SERVICE GPS2 needs service. Return unit f repair. NAV1 SERVICE NAV1 needs service. Return unit f repair. NAV2 SERVICE NAV2 needs service. Return unit f repair. NAV1 RMT XFR NAV1 remote transfer key is stuck. NAV2 RMT XFR NAV2 remote transfer key is stuck. G/S1 FAIL G/S1 is inoperative. G/S2 FAIL G/S2 is inoperative. G/S1 SERVICE G/S1 needs service. Return unit f repair. G/S2 SERVICE G/S2 needs service. Return unit f repair. Abt approach due to loss of GPS navigation. Displayed after passing the first waypoint of a true nth approach when the nav angle is set to AUTO. A failure has been detected in the GPS1 and/ GPS2 receiver. The receiver is unavailable. The G1000 system should be serviced. A failure has been detected in the GPS1 and/ GPS2 receiver. The receiver may still be available. The G1000 system should be serviced. A failure has been detected in the NAV1 and/ NAV2 receiver. The receiver may still be available. The G1000 system should be serviced. The remote NAV1 and/ NAV2 transfer switch is stuck in the enabled ( pressed ) state. Press the transfer switch again to cycle its operation. If the problem persists, the G1000 system should be serviced. A failure has been detected in glideslope receiver 1 and/ receiver 2. The G1000 system should be serviced. A failure has been detected in glideslope receiver 1 and/ receiver 2. The receiver may still be available. The G1000 system should be serviced when possible Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

30 GIA 63W Advisies GIA1 CONFIG GIA1 config err. Config service req d. GIA2 CONFIG GIA2 config err. Config service req d. GIA1 CONFIG GIA1 audio config err. Config service req d. GIA2 CONFIG GIA2 audio config err. Config service req d. GIA1 COOLING GIA1 temperature too low. GIA2 COOLING GIA2 temperature too low. GIA1 COOLING GIA1 over temperature. GIA2 COOLING GIA2 over temperature. GIA1 SERVICE GIA1 needs service. Return the unit f repair. GIA2 SERVICE GIA2 needs service. Return the unit f repair. HW MISMATCH GIA hardware mismatch. GIA1 communication halted. HW MISMATCH GIA hardware mismatch. GIA2 communication halted. The GIA1 and/ GIA2 configuration settings do not match backup configuration memy. The system should be serviced. The GIA1 and/ GIA2 have an err in the audio configuration. The system should be serviced. The GIA1 and/ GIA2 temperature is too low to operate crectly. Allow units to warm up to operating temperature. The GIA1 and/ GIA2 temperature is too high. If problem persists, the system should be serviced. The GIA1 and/ GIA2 self-test has detected a problem in the unit. The system should be serviced. A GIA mismatch has been detected, where only one is SBAS capable Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-19

31 GIA 63W Advisies (Cont.) MANIFEST GIA1 software mismatch, communication halted. MANIFEST GIA2 software mismatch, communication halted. MANIFEST GFC software mismatch, communication halted. MANIFEST COM1 software mismatch, communication halted. MANIFEST COM2 software mismatch, communication halted. MANIFEST NAV1 software mismatch, communication halted. MANIFEST NAV2 software mismatch, communication halted. COM1 TEMP COM1 over temp. Reducing transmitter power. COM2 TEMP COM2 over temp. Reducing transmitter power. COM1 CONFIG COM1 config err. Config service req d. COM2 CONFIG COM2 config err. Config service req d. COM1 TEMP COM1 over temp. Reducing transmitter power. COM2 TEMP COM2 over temp. Reducing transmitter power. COM1 SERVICE COM1 needs service. Return unit f repair. COM2 SERVICE COM2 needs service. Return unit f repair. The GIA1 and/ GIA 2 has increct software installed. The system should be serviced. Increct servo software is installed, gain settings are increct. COM1 and/ COM2 software mismatch. The G1000 system should be serviced. NAV1 and/ NAV2 software mismatch. The G1000 system should be serviced. The system has detected an over temperature condition in COM1 and/ COM2. The transmitter is operating at reduced power. If the problem persists, the system should be serviced. COM1 and/ COM2 configuration settings do not match backup configuration memy. The G1000 system should be serviced. The system has detected an over temperature condition in COM1 and/ COM2. The transmitter is operating at reduced power. If the problem persists, the G1000 system should be serviced. The system has detected a failure in COM1 and/ COM2. COM1 and/ COM2 may still be usable. The system should be serviced when possible Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

32 GIA 63W Advisies (Cont.) COM1 PTT COM1 push-to-talk key is stuck. COM2 PTT COM2 push-to-talk key is stuck. COM1 RMT XFR COM1 remote transfer key is stuck. COM2 RMT XFR COM2 remote transfer key is stuck. LOI GPS integrity lost. Crosscheck with other NAVS. GPS NAV LOST Loss of GPS navigation. Insufficient satellites. GPS NAV LOST Loss of GPS navigation. Position err. GPS NAV LOST Loss of GPS navigation. GPS fail. ABORT APR Loss of GPS navigation. Abt approach. APR DWNGRADE Approach downgraded. TRUE APR True nth approach. Change HDG reference to TRUE. GPS1 SERVICE GPS1 needs service. Return unit f repair. GPS2 SERVICE GPS2 needs service. Return unit f repair. NAV1 SERVICE NAV1 needs service. Return unit f repair. NAV2 SERVICE NAV2 needs service. Return unit f repair. The COM1 and/ COM2 external push-to-talk switch is stuck in the enable ( pressed ) position. Press the PTT switch again to cycle its operation. If the problem persists, the system should be serviced. The COM1 and/ COM2 transfer switch is stuck in the enabled ( pressed ) position. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. GPS integrity is insufficient f the current phase of flight. Loss of GPS navigation due to insufficient satellites. Loss of GPS navigation due to position err. Loss of GPS navigation due to GPS failure. Abt approach due to loss of GPS navigation. Vertical guidance generated by SBAS is unavailable, use LNAV only minimums. Displayed after passing the first waypoint of a true nth approach when the nav angle is set to AUTO. A failure has been detected in the GPS1 and/ GPS2 receiver. The receiver may still be available. The system should be serviced. A failure has been detected in the NAV1 and/ NAV2 receiver. The receiver may still be available. The system should be serviced Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-21

33 GIA 63W Advisies (Cont.) NAV1 RMT XFR NAV1 remote transfer key is stuck. NAV2 RMT XFR NAV2 remote transfer key is stuck. G/S1 FAIL G/S1 is inoperative. G/S2 FAIL G/S2 is inoperative. The remote NAV1 and/ NAV2 transfer switch is stuck in the enabled ( pressed ) state. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. A failure has been detected in glideslope receiver 1 and/ receiver 2. The system should be serviced. G/S1 SERVICE G/S1 needs service. Return unit f repair. G/S2 SERVICE G/S2 needs service. Return unit f repair. FAILED PATH A data path has failed. GEA 71 Advisies GEA1 CONFIG GEA1 config err. Config service req d. MANIFEST GEA1 software mismatch, communication halted. GSR 56 Advisies GSR1 FAIL GSR1 has failed. GDC 74A Advisies ADC1 ALT EC ADC1 altitude err crection is unavailable. ADC1 AS EC ADC1 airspeed err crection is unavailable. MANIFEST GDC1 software mismatch, communication halted. A failure has been detected in glideslope receiver 1 and/ receiver 2. The receiver may still be available. The system should be serviced when possible. A data path connected to the GDU the GIA 63/W has failed. The GEA1 configuration settings do not match those of backup configuration memy. The G1000 system should be serviced. The #1 GEA 71 has increct software installed. The G1000 system should be serviced. A failure has been detected in the #1 GSR 56. The system should be serviced. GDC1 is repting that the altitude err crection is unavailable. GDC1 is repting that the airspeed err crection is unavailable. The GDC 74A has increct software installed. The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A

34 GTX 33 Advisies XPDR1 CONFIG XPDR1 config err. Config service req d. MANIFEST GTX1 software mismatch, communication halted. XPDR1 SRVC XPDR1 needs service. Return unit f repair. XPDR1 FAIL XPDR1 is inoperative. The transponder configuration settings do not match those of backup configuration memy. The system should be serviced. The transponder has increct software installed. The system should be serviced. The #1 transponder should be serviced when possible. There is no communication with the #1 transponder. GRS 77 Advisies AHRS1 TAS AHRS1 not receiving airspeed. AHRS1 GPS AHRS1 using backup GPS source. AHRS1 GPS AHRS1 not receiving any GPS infmation. AHRS1 GPS AHRS1 not receiving backup GPS infmation. AHRS1 GPS AHRS1 operating exclusively in no-gps mode. AHRS1 SRVC AHRS1 Magneticfield model needs update. GEO LIMITS AHRS1 too far Nth/South, no magnetic compass. MANIFEST GRS1 software mismatch, communication halted. The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS infmation to augment the lack of airspeed. The system should be serviced. The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible. The #1 AHRS is not receiving any any useful GPS infmation. Check AFMS limitations. The system should be serviced. The #1 AHRS is not receiving backup GPS infmation. The system should be serviced. The #1 AHRS is operating exclusively in no-gps mode. The system should be serviced. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The aircraft is outside geographical limits f approved AHRS operation. Heading is flagged as invalid. The #1 AHRS has increct software installed. The system should be serviced Rev. A Garmin G1000 Cockpit Reference Guide f the Cessna Nav III 13-23

35 GMU 44 Advisies HDG FAULT AHRS1 magnetometer fault has occurred. MANIFEST GMU1 software mismatch, communication halted. A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS f backup mode operation. The G1000 system should be serviced. The GMU 44 has increct software installed. The G1000 system should be serviced. GDL 69/69A Advisies GDL69 CONFIG GDL 69 config err. Config service req d. GDL69 FAIL GDL 69 has failed. MANIFEST GDL software mismatch, communication halted. Miscellaneous Advisies FPL WPT LOCK Flight plan waypoint is locked. FPL WPT MOVE Flight plan waypoint moved. TIMER EXPIRD Timer has expired. DB CHANGE Database changed. Verify user modified procedures. DB CHANGE Database changed. Verify sted airways. GDL 69 configuration settings do not match those of backup configuration memy. The G1000 system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced The GDL 69 has increct software installed. The G1000 system should be serviced. Upon power-up, the system detects that a sted flight plan waypoint is locked. This occurs when an navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted. Remove the waypoint from the flight plan if it no longer exists in any database, Or update the waypoint name/identifier to reflect the new infmation. The system has detected that a waypoint codinate has changed due to a new navigation database update. Verify that sted flight plans contain crect waypoint locations. The system notifies the pilot that the timer has expired. This occurs when a sted flight plan contains procedures that have been manually edited. This alert is issued only after an navigation database update. Verify that the user-modified procedures in sted flight plans are crect and up to date. This occurs when a sted flight plan contains an airway that is no longer consistent with the navigation database. This alert is issued only after an navigation database update. Verify use of airways in sted flight plans and reload airways as needed Garmin G1000 Cockpit Reference Guide f the Cessna Nav III Rev. A