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190-01255-00 Rev. B
Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
484
APPENDIX A
Annunciation Text Description Audio Alert
MGT MISCOMP MGT miscompare event.
Single Ping
NG EXCEED Engine Ng is in exceedance.
NG MISCOMP Ng miscompare event.
NP EXCEED Engine NP is in exceedance.
NP MISCOMP NP miscompare event.
NR MISCOMP NR miscompare event.
PEDAL STOP Pedal stop check or failed to engage or disengage upon command. Or, loss
of ADC inputs.
Q EXCEED Engine torque is in exceedance.
Q MISCOMP Q miscompare event.
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.
ADVISORY MESSAGES
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 self 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.
SAFE OPERATING ANNUNCIATION
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.