Pilot's Guide

Garmin G1000H
™
Pilot’s Guide for the Bell 407GX
190-01255-01 Rev. A98
ENGINE INDICATION & CREW ALERTING SYSTEM
Annunciation Text Description Audio Alert
R/FUEL XFR Right fuel transfer pump has failed.
SLIDING DOOR Left or right Sliding Door not securely closed Single Ping
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
Annunciation Text Description
ALTN DATA FAIL Alternate engine data source is not available.
AUTO RELIGHT Engine igniter is operating.
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.
LASER FIRE Laser Fire operating.
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.
LASER ARMED
Laser Armed.
QUIET MODE ON
Engine Quiet Mode is on.
WOG
Aircraft is on the ground.
Table 3-4 Safe Operating Advisory CAS Messages