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Indicates that the affected engine turbine has overheated.
L.R FADEC FAIL
Indicates that there is a failure of both lanes in the affected FADEC. Engine operation may be affected.
L.R ENG SAV FAIL
Indicates that the affected engine start air valve has failed.
L.R OIL LO PRESS
Indicates that the affected engine has low oil pressure, while the engine is operating.
A/T NOT IN HOLD
Indicates that the A/T is not in take-off hold mode above 60 knots during take-off roll until transitioning through 400 feet AGL.
GF1810_099
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
POWER PLANT
L.R FUEL LO PRESS
Indicates that the affected engine has low fuel feed pressure with the HPSOV open.
L.R FADEC N1 CTL
Indicates that the affected engine is in N1 control. FADEC has detected a fault and has reverted to N1 control.
L.R FADEC OVHT
Indicates that the affected engine’s FADEC internal temperature monitor has tripped.
L and R FUEL FILTER
Indicates that both engines
have impending fuel filter bypass.
L.R OIL LO QTY
Indicates that the affected engine’s oil quantity is low.
L.R REVERSER FAIL
Indicates that the affected reverser has failed and the doors will remain in current position.
L.R REV LOCK FAIL
Indicates that 2 of 3 reverser locks, on the affected reverser, are not locked, with the thrust lever in the forward position.
L.R THROTTLE FAIL
Indicates that the affected thrust lever has failed. Engine operation will be affected and corresponding thrust reverser will not deploy.
L.R START ABORTED
Indicates that FADEC has aborted the affected engine start.
GF1810_100
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
POWER PLANT
POWER PLANT EICAS MESSAGES (CONT'D)
A/T 1 (2) FAIL
Indicates that the A/T is invalid, or reporting a hardware or servo
A/T ADC MISCOMP
Indicates that the A/T isis available due to an ADC data miscompare.
ENG SYNC FAIL
Indicates that the affected
SYNC system has failed.
L (R) FUEL FILTER
Indicates that the affected fuel
filter is impending bypass.
A/T IRS MISCOMP
Indicates that the A/T is not available due to an IRS data miscompare.
L (R) OIL FILTER
Indicates that the affected oil
filter is impending bypass.
L (R) REVERSER FAULT
Indicates that there is a minor fault in the affected thrust reverser system. Engine operation should be normal.
L (R) REV LOCK FAULT
Indicates that one of two primary stow switches, on affected thrust reverser, is indicating not stowed,
has < 1.5 quarts of oil remaining. with the thrust lever in the forward
WINDMILL ENVELOPE
range.
Indicates that FADEC has determined that the airplane is within the windmill start envelope.
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