Table 20.Engine Cas Messages - Eclipse 500 System Manual

Section 8. Engines & Fire Protection
8.8 Crew Alerting System Messages
Message
L (R) ENG FAIL
L (R) ENG FIRE
L (R) ENG EXCEEDANCE
L (R) ENG OIL TEMP HIGH
L (R) ENG OIL PRESS HIGH
L (R) ENG OIL PRESS LOW
L (R) ENG FUEL HOT
ENG START ABORT
L (R) ENG CONTROL FAIL
L (R) ENG OIL TEMP HIGH
L (R) ENG OIL TEMP LOW
L (R) ENG CHIP DETECTED
L (R) ENG CHIP FAULT
L (R) ENG CONTROL
L (R) ENG OIL BYPASS
FAULT
L (R) ENG OIL FILTER
L (R) ENG OIL TEMP FAULT
ENG START FAIL
L (R) EXTNGR DSCHG
L (R) FIRE DETECTOR
FAULT
APR DISARMED
178
Table 20. Engine CAS Messages
Condition
Left or Right Engine failure
Engine fire detected
Engine has exceeded limits (N1, N2, ITT,
expiration of 5 minute T/O thrust or 10 minute APR
ON timer.)
Oil temperature exceeds allowable limits
Oil pressure exceeds allowable limits
Oil pressure below allowable limit
Fuel temperature at engine Fuel Metering Unit
(FMU) exceeds limits
Engine start aborted by FADEC (ground only)
A failure has occurred in the engine control system
that may degrade engine control. The engine may
fail to a fixed fuel flow or throttle setting
Oil temperature is between 135°C and 140°C
Oil temperature below 20°C (ground only)
Metal particles detected in engine oil (ground only)
Engine oil chip detector has failed and may not be
ale to detect metal in the engine oil (ground only)
A loss of redundancy in the engine control system
has occurred. Engine operation is not affected.
(ground only)
The engine oil filter bypass pressure switch failure
(ground only)
The engine oil filter pressure switch has tripped,
the oil filter may be bypassed (ground only)
Engine oil temperature sensor failure. (ground
only)
Aircraft systems did not automatically configure for
start
Left or right fire extinguisher has discharged.
Once discharged, the fire extinguisher capability
has been depleted
Fire detection circuit is shorted or open. Fire
detection is unavailable.
APR disarmed (ground only)
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Version 2.0 April 2007