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Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
190-01255-00 Rev. B92
ENGINE INDICATION & CREW ALERTING SYSTEM
Annunciation Text Description Audio Alert
Q MISCOMP Q miscompare event.
Single Ping
R/FUEL BOOST Right fuel boost pump has failed.
R/FUEL XFR Right fuel transfer pump has failed.
T/R CHIP T/R Chip Detector has detected debris.
XMSN CHIP Transmission Chip Detector has detected debris in transmission oil.
Table 3-2 Caution CAS Messages
NOTE: See the Rotorcraft Flight Manual (RFM) for recommended pilot actions.
Annunciation Text Description
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 Description
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