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Volume 2
18−10−66
POWER PLANT EICAS MESSAGES
GF1810_099
DUAL ENGINE OUT
L OIL LO PRESS
R OIL LO PRESS
L REVERSER UNLKD
R REVERSER UNLKD
A/T NOT IN HOLD
L ENG FLAMEOUT
R ENG FLAMEOUT
L ENG FUEL LO TEMP
R ENG FUEL LO TEMP
L ENG OVERSPED
R ENG OVERSPED
L ENG OVHT
R ENG OVHT
L ENG SAV FAIL
R ENG SAV FAIL
L FADEC FAIL
R FADEC FAIL
L−R OIL LO PRESS
Indicates that the affected
engine has low oil pressure,
while the engine is operating.
L−R REVERSER UNLKD
Indicates that the affected
reverser is unlocked, with
the thrust lever in the forward
L−R ENG FLAMEOUT
Indicates that there is a flameout
on the affected engine.
L−R ENG FUEL LO TEMP
Indicates that the affected engine
fuel inlet temperature is
approaching the fuel freezing point.
L−R ENG OVHT
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 ENG OVERSPED
Indicates that the affected engine
shut down caused by independent
overspeed protection.
A/T NOT IN HOLD
Indicates that the A/T is not in takeoff
hold mode above 60 knots during
takeoff
roll until transitioning through
400 feet AGL.
DUAL ENGINE OUT
Indicates that a flameout has been
detected in both the L and R
engine or both L and R engines
are shutdown (in flight).
position.
POWER PLANT
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
18−10−67
POWER PLANT EICAS MESSAGES (CONT'D)
GF1810_100 L
FADEC N1 CTL
R FADEC N1 CTL
L FADEC OVHT
R FADEC OVHT
L−R FUEL FILTER
L FUEL LO PRESS
R FUEL LO PRESS
L OIL LO QTY
R OIL LO QTY
L REVERSER FAIL
R REVERSER FAIL
L REV LOCK FAIL
R REV LOCK FAIL
L START ABORTED
R START ABORTED
L THROTTLE FAIL
R THROTTLE FAIL
L and R FUEL FILTER
Indicates that both engines
have impending fuel filter bypass.
L−R FUEL LO PRESS
Indicates that the affected engine
has low fuel feed pressure with
the HPSOV open.
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 START ABORTED
Indicates that FADEC has
aborted the affected engine start.
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 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 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.
POWER PLANT
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
18−10−68
POWER PLANT EICAS MESSAGES (CONT'D)
GF1810_101
ATS ENVELOPE
L FADEC FAULT
R FADEC FAULT
L FUEL FILTER
R FUEL FILTER
L OIL FILTER
R OIL FILTER
L REVERSER FAULT
R REVERSER FAULT
L REV LOCK FAULT
R REV LOCK FAULT
OIL RES LO QTY
WINDMILL ENVELOPE
ATS ENVELOPE
Indicates that FADEC has determined
that the airplane is within the starter
L−R FADEC FAULT assisted engine relight envelope.
Indicates that there is a minor fault
in the affected FADEC. Engine
operation should not be affected.
L−R FUEL FILTER
Indicates that the affected fuel
filter is impending bypass.
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, with
the thrust lever in the forward range.
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