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Indicates that RUN is
Indicates that an APU
APU SHUTDOWN
than 3.3 psia (35,000 ft).
The 60 second warm-up
protective shut downperiod after speed reaches
has occurred, other 99% is not complete
than an overspeed or(ground only).
over temperature.
2 . When there is an invalid bleed configuration such as:
APU IN BITE
Both R PRV and xbleed selected and thevalve are open at the prestart BITE is insame time progress.
or
ICE ON (either L or R
Wing A-Ice open)
APU BLEED ON
or Indicates that the APU
L PRV open BLEED switch is in the ON position and the load control valve is open.
APU FAULT
Indicates a failure in
APU BLEED OFF
one of the following: Indicates that the APU
Single speed BLEED switch is in the
sensor.
OFF position and the
EGT thermocouple.
load control valve is
closed.
Fuel solenoid (failed
to close).
Fuel/oil filters in
impending by-pass. APU SOVS CLSD APU FUEL SOV CLSD
Indicates that both fuel Indicates that the APU
Low oil pressure
and bleed air shutoff fuel shutoff valve is
switch has failed
valves are closed. closed.
(in flight).
GF0510_018b
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
AUXILIARY POWER UNIT EMS CIRCUIT PROTECTION
CB - APU SYSTEM
CB . APU SYSTEM 1/1
APU DOOR APU BATT ASCA IN
APU FADEC PWR 1 BATT IN
APU FADEC PWR 2 AV BATT DCPC IN
APU OIL HEAT AC 4 IN
APU START BATT IN
APU START CONTACT APU BATT ASCA IN
GF0520_001
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
AUXILIARY POWER UNIT
EMS CIRCUIT PROTECTION
THIS PAGE INTENTIONALLY LEFT BLANK
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
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本文链接地址：庞巴迪环球5000公务机机组操作手册 Bombardier Global-辅助动力装置(14)
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