Garmin G1000H Bell 407GX Pilot's Guide - Page 104
Table 3-2, Caution CAS Messages, Table 3-4 Safe Operating Advisory CAS Messages, ALTN DATA FAIL
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ENGINE INDICATION & CREW ALERTING SYSTEM Annunciation Text Q MISCOMP R/FUEL BOOST R/FUEL XFR T/R CHIP XMSN CHIP Description 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 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 Audio Alert Single Ping 92 Garmin G1000H™ Pilot's Guide for the Bell 407GX 190-01255-00 Rev. A