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
To re-establish normal operations:
(2) ADG manual release handle ................................Select to STOW (if ADG was
manually deployed).
(3) ADG PWR TXFR OVERRIDE
switch .................................................................Push in to override.
(4) HYDRAULIC pump switch 3B ..............................Check selected to AUTO.
NOTE
For flight planning, a fuel burn correction of 5% should be used when
the ADG is deployed.
END
G. APU Battery Failure
Indication: APU BATTERY OFF caution message on. DC ELECTRICAL page – APU
battery indicates less than 18 volts DC.
(1) BATT MASTER switch .........................................Check ON.
(2) DC ELECTRICAL page ......................................Monitor APU battery voltage. Assume
loss of APU battery. The APU
is not available.
(3) Affected airplane systems .................................. Review Refer to Bus Inoperative List
in this section.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−3
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
H. APU Generator Failure
Indication: APU GEN OFF caution message on.
(1) AC POWER, APU GEN switch.............................Select to OFF/RESET then ON.
APU GEN OFF caution message persists:
Yes
(2) AC POWER, APU GEN
switch............................................................Select to OFF.
(3) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) AC ELECTRICAL page ......................................Monitor loads on APU generator.
END
I. APU Generator Overload
Indication: APU GEN OVLD caution message on. AC ELECTRICAL page – APU
generator load readout is greater than 35 KVA.
(1) AC ELECTRICAL page ......................................Monitor load on APU generator.
(2) AC loads............................................................ Reduce as necessary.
END
J. Battery Bus Failure
Indication: BATTERY BUS caution message on.
(1) Land at the nearest suitable airport.
(2) Affected airplane systems .................................. Review Refer to Bus Inoperative List
in this section.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−4
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
K. DC BUS 1 Failure
Indication: DC BUS 1 caution message on. DC ELECTRICAL page – DC BUS 1
inoperative.
(1) DC POWER, MAIN BUS TIE
switch/light .........................................................Press in to close bus tie manually.
Check MAIN BUS TIE
CLOSED light on.
DC BUS 1 caution message persists:
Yes
(2) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) No further action required.
END
L. DC BUS 2 Failure
Indication: DC BUS 2 caution message on. DC ELECTRICAL page – DC BUS 2
inoperative.
(1) DC POWER, MAIN BUS TIE
switch/light .........................................................Press in to close bus tie manually.
Check MAIN BUS TIE
CLOSED light on.
DC BUS 2 caution message persists:
Yes
(2) Affected airplane systems .......................... Review Refer to Bus Inoperative List
in this section.
− END −
No
(2) No further action required.
END
M. DC Essential Bus Failure
Indication: DC ESS BUS caution message on. DC ELECTRICAL page − DC ESS BUS
inoperative.
(1) Land at the nearest suitable airport.
(2) Affected airplane systems .................................. Review Refer to Bus Inoperative List
in this section.
END
ABNORMAL PROCEDURES
Electrical
Vol. 1 05−09−5
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. ELECTRICAL (CONT'D)
N. AC Generator 1 Failure
Indication: GEN 1 OFF caution message on.
(1) AC POWER, GEN 1 switch ..................................Select to OFF/RESET then ON.
GEN 1 OFF caution message persists:
Yes
(2) AC POWER, GEN 1 switch ..........................Select to OFF.
NOTE
1. With generator 1 shutdown, HYD PUMP 2B is load
shed.
2. During single generator operations, AC utility busses
are shed, unless on ground with flaps at 0°.
(3) APU (if available)............................................ Start when at or below 20,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者604操作手册 Operating Manual 2(5)
