Garmin G1000H Bell 407GX Pilot's Guide - Page 492

APPENDIX A Annunciation Text MGT MISCOMP NG EXCEED NG MISCOMP NP EXCEED NP MISCOMP NR MISCOMP PEDAL STOP Q EXCEED Q MISCOMP R/FUEL BOOST R/FUEL XFR T/R CHIP XMSN CHIP Description MGT miscompare event. Engine Ng is in exceedance. Ng miscompare event. Engine NP is in exceedance. NP miscompare event. NR miscompare event. Pedal stop check or failed to engage or disengage upon command. Or, loss of ADC inputs. Engine torque is in exceedance. 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. ADVISORY MESSAGES See the Rotorcraft Flight Manual (RFM) for recommended pilot actions. Annunciation Text ALTN DATA FAIL AUTO RELIGHT ENG ANTI-ICE FADEC MAINT INSTR FAN NG OAT LIMIT QUIET MODE SEL RESTART FAULT START Description Alternate engine data source is not available. FADEC is attempting to perform an auto relight. Engine Anti-Ice valve is open, pressure is high. FADEC lamp test failure during power-up self test and in flight. Instrument panel area fan has failed. Engine Ng limited due to OAT. Quiet Mode switch is in quiet position. ECU fault will not allow start in AUTO (ECU) Mode. Engine starter is engaged. SAFE OPERATING ANNUNCIATION Annunciation Text FLOAT TEST QUIET MODE ON WOG Float system is in test mode. Engine Quiet Mode is on. Aircraft is on the ground. Description Audio Alert Single Ping 480 Garmin G1000H™ Pilot's Guide for the Bell 407GX 190-01255-00 Rev. A