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exceedance data shall be the time the parameter was within its defined exceedance band, if any, up
to 5 minutes maximum.
If an exceedance event is detected a data set is stored automatically by the Fault Warning Computer
(FWC). A data set is also stored when the PILOT EVENT button is selected. A data set consists of
parameters recorded every second spanning from 10 seconds prior to the exceedance event, the
parameters when the event was triggered, and concluding 19 seconds after the event.
GF1810_098
PILOT EVENT
Button
Landing Gear Control Panel
NOSE STEER LDG GEAR
HORN PILOT
EVENT
MUTED
POWER PLANT
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
18−10−68
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 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
18−10−69
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 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
18−10−70
POWER PLANT EICAS MESSAGES (CONT'D)
GF1810_101a
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
　
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