Page 289 - (KU)01-75GAJ-1.5 - Change 1
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INTRO
EP'S (KU)01-75GAJ-1.5 FIGURES
1.10.1 ELECTRICAL SYSTEMS FAILURE
ACAWS
WARNING
GROUND
Do not operate the aircraft without serviceable batteries.
3RZHU ZRXOG QRW EH DYDLODEOH WR RSHUDWH WKH ¿UH TAKEOFF
extinguisher system, alarm bells, standby instruments,
emergency exit lights extinguish, utility lights or smoke
detectors. FIRE/SMK
NORM ,W LV H[WUHPHO\ GLI¿FXOW WR DQWLFLSDWH DOO WKH SRVVLEOH HOHFWULFDO IDLOXUHV
and to plan corrective action and procedures for each failure. However, PRES/OXY
NOT FOR FLIGHT
a broad analysis of the situation indicates that failures fall into three
possible categories:
ENG/PROP
Loss of one or more of the primary power sources.
Faults on the main bus or distribution system.
FUEL
Faults within equipment items.
Faults in the distribution system and load circuits are controlled through
protective devices such as circuit breakers, fuses and current limiters. AAR
Should one of these devices fail to operate, considerable smoke can result
SPEC and some emergency action on the part of the crew may be needed. ELEC
CAUTION
HYD
When isolating or restoring 3-phase AC power, ensure
all three MCBs are pulled or reset. FLT CTRL
(End of Procedure)
GEAR
1.10.2 PARTIAL LOSS OF ELECTRICAL SYSTEMS DOR/RMP
PERF Utility Battery bus powers:
Alarm bells JETTISON
APU emergency start
AV BAT control LANDING
DC voltmeter (utility battery)
Emergency exit light extinguish DITCHING
FADECs 2 and 3 (starting)
Emergency engine shutdown 2 and 3 BAILOUT
Fire bottles 1 and 2, and control
OPER FAULT LG
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