曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
12-01-12 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
Sep 14/2005 Flight Crew Operating Manual Volume 2 REV 4 CSP 100-6
12-01-13 EICAS MESSAGES (Cont)
MESSAGE INHIBITS MEANING AURAL WARNING
FUEL QUANTITY FAULT TO/LAND The left or right channel has detected a fault or loss of temperature compensation
FUEL XFER FAIL TO/LAND The fuel transfer valve has failed
L (R) ENG FUEL SOV CLOSED Respective engine fuel shutoff valve is closed
FUEL BALANCED TO/LAND The fuel is balanced within 100 lb with the FUEL XFER valve open
FUEL GRAV XFLOW OPEN Wing fuel gravity crossflow valve is open
L (R) FUEL PUMP OFF The respective fuel pump is OFF
L (R) FUEL PUMP ON The respective fuel pump is ON
FUEL XFER OPEN The fuel transfer valve is open
Volume 2 Flight Crew Operating Manual Sep 14/2005 CSP 100-6 REV 4
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-燃油(10)
| 
