BOMBARDIER BD-100-1A10, Руководство по эксплуатации

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FUEL
Sep 14/2005 Flight Crew Operating Manual Volume 2
REV 4 CSP 100-6
12-01-13
EICAS MESSGAES
The fuel system messages are shown on the EICAS. In the table below, the fuel system messages and inhibits are listed.
A brief explanation of each messages is provided.
MESSAGE INHIBITS MEANING
AURAL
WARNING
L (R) ENG FUEL SOV
FAIL
TO/LAND
The respective engine fuel shutoff valve has
failed to close when commanded
L (R)
FUEL COLLECTOR
LOW
TO
The fuel collector tank quantity is less than 200
pounds
L (R) FUEL EJECTOR
FAIL
TO/LAND
The affected ejector pump has failed to provide
sufficient pressure.
FUEL IMBALANCE TO/LAND
The wing fuel imbalance is greater than:
- 250 lb (113 kg) with a total fuel weight of more
than 13 700 lb (6214 kg)
- 315 lb (143 kg) with a total fuel weight between
13 700 lb (6214 kg)
- 450 lb (204 kg) with a total fuel weight between
10 000 lb (4536 kg)
- 600 lb (272 kg) with a total fuel weight of less
than 4700 lb (2132kg)
L (R) FUEL PRESSURE
LOW
The engine fuel pressure is below 6 psig
L (R) FUEL PUMP FAIL TO/LAND The respective electric fuel pump has failed
FUEL QUANTITY FAIL TO/LAND
Both channels of the fuel quantity gauging com-
puter have failed. fuel quantities will be indi-
cated as magenta dashes on the EICAS
FUEL QUANTIT Y LOW
Total fuel quantity is 300 lb (136 kg) or less in
either wing, when the aircraft is in unaccelerated
level flight
WING FUEL TEMP
LOW
TO/LAND
Fuel temperature in the wing is below
-38
°
C (-36
°
F)
L (R) FUEL EJECTOR
FAIL
TO/LAND
The affected ejector pump has failed to provide
sufficient pressure. The electric fuel pump
should automatically turn on to provide sufficient
fuel pressure.
FUEL GRAV XFLOW
FAIL
TO/LAND
The wing fuel gravity crossflow valve is not fully
opened or closed as commanded
L (R) FUEL PUMP ON
The respective electric fuel pump has been
automatically turned on
REV 4