Garmin G1000H Pilot's Manual page 103
Integrated flight deck pilot’s guide for the bell 407gx
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Also See for G1000H:
- Cockpit reference manual (136 pages) ,
- Cockpit reference manual (158 pages)
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See the Rotorcraft Flight Manual (RFM) for recommended pilot actions.
NOTE:
Annunciation Text
BATTERY HOT
ENGINE FIRE
ENGINE OUT
ENGINE OVSPD
FADEC FAIL
XMSN OIL PRESS
XMSN OIL TEMP
Annunciation Text
BAGGAGE DOOR
BATTERY RLY
ENGINE CHIP
FADEC DEGRADED
FADEC FAULT
FADEC MANUAL
FLOAT ARM
FUEL FILTER
FUEL LOW
FUEL VALVE
GEN FAIL
HEATER OVERTMP
HYDRAULIC SYS
L/FUEL BOOST
L/FUEL XFR
LITTER DOOR
MGT EXCEED
MGT MISCOMP
NG EXCEED
NG MISCOMP
NP EXCEED
NP MISCOMP
NR MISCOMP
PEDAL STOP
Q EXCEED
190-01255-00 Rev. A
Description
Battery overheat detected.
Fire/Overheat detector senses a temperature greater than or equal to 338°F.
Ng less than 55% or FADEC senses engine out.
Ng greater than 110% or NP vs torque is above maximum continuous limit.
Both the primary and reversionary channels have failed.
Transmission oil pressure is low.
Transmission oil overheat is detected.
Table 3-1 Warning CAS Messages
Baggage door is not securely latched.
Battery relay energized when battery switch is off. Battery still connected to DC bus.
Chip detector has detected debris in engine oil.
FADEC fault detected that may result in degraded engine performance.
A fault is recorded in the FADEC.
FADEC is in manual mode.
Floats Arm switch is in the armed position.
External fuel filter is partially blocked before impending bypass.
Fuel feed tank sensor indicates low fuel. 100 ± 10 pounds of fuel remain in aft tank.
Fuel valve is in transition or is not in the commanded position.
Generator not connected to DC bus.
An over temperature condition has been detected either under the pilot's seat, copilot's seat, or
in the vertical tunnel.
Low pressure in hydraulic system.
Left fuel boost pump has failed.
Left fuel transfer pump has failed.
Litter door is not securely latched.
MGT is in exceedance.
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.
Garmin G1000H
™
ENGINE INDICATION & CREW ALERTING SYSTEM
Description
Pilot's Guide for the Bell 407GX
Audio Alert
Single Chime
Continuous Chime
Continuous Fast-Pulsing Chime
Single Chime
Repeating Ding-Dong Chime
Single Chime
Single Chime
Audio Alert
Single Ping
91
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