Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
190-01255-00 Rev. A
92
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
Содержание G1000H
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