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This indicates a loss of the CAS messaging system. This is usually caused by a
database or configuration mismatch within the G1000 system after loading software.
• ON GROUND
1. Correct prior to flight.
PROCEDURE COMPLETED
• IN FLIGHT
1. Land as soon as practical.
C A U T I O NCAUTION
No CAS messages will post to indicate any emergency, abnormal or normal
system conditions.
PROCEDURE COMPLETED
2  PIT/ROL/HDG MISCOMP (PITCH/ROLL/HEADING
MISCOMPARE)
3  CAS FAILURE (RED “X” ON CAS MESSAGE WINDOW)
510CLEAP-07 AA 65
T
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
This is indicated by a complete loss of image on a display. If only individual
elements of the display are failed, refer to appropriate procedures for the individual
failures.
• IF PFD
1. DISPLAY BACKUP Button (affected side) - - - - - PRESS, IF REQUIRED
(flight and EICAS information is displayed on MFD)
2. Flight Director - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TRANSFER
(XFR button) to operating PFD
3. FD Modes/AUTOPILOT - - - -RESELECT and REENGAGE as required
4. Transponder - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SWITCH
to operating transponder
5. COM and NAV Radios- - - - - - - - - - - - - - - - - - - - - - - - - - - - - SWITCH
to operating Com and Nav radios.
6. PFD Controls - - - - - - - - - - - - - - - - - - - - - - - - - USE OPERATING PFD
for required data entry (Com, Nav, Baro setting, etc.)
C A U T I O NCAUTION
The “FUEL LO INOP L-R” and the “PRESS CTRL” messages may be
displayed. Refer to the abnormal procedures for these messages as time
allows.
PROCEDURE COMPLETED
• IF MFD
1. Either DISPLAY BACKUP Button - - - - - - - - - - - - - - - - - - - - - - PRESS
(EICAS info will be displayed on PFDs)
PROCEDURE COMPLETED
Audio panel failure may be indicated by a GMA 1/2 FAIL Garmin System Message
or the inability to communicate using the affected audio panel. This failure may also
be accompanied by the loss of some aural warnings such as Altitude Alert, Autopilot
Disconnect, TAWS and Traffic alerts.
1. AUDIO1 or AUDIO2 Circuit Breaker (affected side)- - - - - - - - - - - - - -PULL
2. SPKR Button (operating audio panel) - - - - - - - - - - - - - - - - - - - - - - - - ON
3. COM Radio - - - - - - - - - - - - - - - - - - - - - - - - - - - - -USE ON-SIDE RADIO
for communication (Pilot-COM1, Copilot-COM2)
PROCEDURE COMPLETED
1  DISPLAY UNIT FAILURE
2  AUDIO PANEL FAILURE
66 AA 510CLEAP-07
U
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
When both GPS receivers are inoperative, the G1000 system will enter one of two
modes: Dead Reckoning mode (DR) or Loss Of Integrity mode (LOI). The mode is
indicated on the HSI by an amber “DR or “LOI”. Which mode is active depends on the
distance from the destination airport in the active flight plan.
• IF ALTERNATE NAVIGATION SOURCES (ILS, LOC, VOR, DME, ADF)
ARE AVAILABLE
1. Navigation - - - - - - - - - - - - - - - - - - - - - - USE ALTERNATE SOURCES
PROCEDURE COMPLETED
• IF NO ALTERNATE NAVIGATION SOURCES ARE AVAILABLE
 DEAD RECKONING (DR) MODE - ACTIVE WHEN THE AIRPLANE
IS GREATER THAN 30 NM FROM THE DESTINATION AIRPORT.
1. Navigation - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -USE
the airplane symbol and magenta course line on the map display
WARNING
• All information normally derived from GPS turns amber. All of this
information will become more inaccurate over time.
• TAWS is inoperative.
 LOSS OF INTEGRITY (LOI) MODE - ACTIVE WHEN THE AIRPLANE
IS WITHIN 30NM OF THE DESTINATION AIRPORT (AS
CALCULATED FROM THE PREVIOUS GPS OR DR POSITION).
1. Navigation - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLY
towards known visual conditions or available terminal navigation
sources. Use ATC or other information sources as possible.
PROCEDURE COMPLETED
1. COM Frequency Toggle Button (affected PFD) - - - - - - - - - - - - - - -PRESS
AND HOLD FOR 2 SECONDS
PROCEDURE COMPLETED
1. TRANSPONDER)- - - - - - - - - - - - - SELECT OPPOSITE TRANSPONDER
a. PFD XPDR Softkey - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
b. XPDR1 or XPDR2 Softkey - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
to select opposite transponder
2. XPDR1 or XPDR2 Circuit Breaker (affected side) - - - - - - - - - - - - - - - PULL
PROCEDURE COMPLETED
3  DUAL GPS FAILURE (AMBER “DR”OR “LOI” ON HSI)
　
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