Garmin G1000H Pilot's Manual page 104

ENGINE INDICATION & CREW ALERTING SYSTEM
Annunciation Text
Q MISCOMP
R/FUEL BOOST
R/FUEL XFR
T/R CHIP
XMSN CHIP
See the Rotorcraft Flight Manual (RFM) for recommended pilot actions.
NOTE:
Annunciation Text
92
Q miscompare event.
Right fuel boost pump has failed.
Right fuel transfer pump has failed.
T/R Chip Detector has detected debris.
Transmission Chip Detector has detected debris in transmission oil.
Table 3-2 Caution CAS Messages
ALTN DATA FAIL Alternate engine data source is not available.
AUTO RELIGHT
FADEC is attempting to perform an auto relight.
ENG ANTI-ICE
Engine Anti-Ice valve is open, pressure is high.
FADEC MAINT FADEC lamp test failure during power-up test and in flight.
INSTR FAN
Instrument panel area fan has failed.
NG OAT LIMIT Engine Ng limited due to OAT.
QUIET MODE SEL Quiet Mode switch is in quiet position.
RESTART FAULT
ECU fault will not allow start in AUTO (ECU) Mode.
START Engine starter is engaged.
Table 3-3 Advisory CAS Messages
Annunciation Text
FLOAT TEST
Float system is in test mode.
QUIET MODE ON
Engine Quiet Mode is on.
WOG Aircraft is on the ground
Table 3-4 Safe Operating Advisory CAS Messages
Garmin G1000H
™
Description
Description
Description
Pilot's Guide for the Bell 407GX
Audio Alert
Single Ping
190-01255-00 Rev. A