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GROUND
SPOILERS
NO NO
HF #1 NO #2 NO
IRU #1 OK
IF L
MAIN
AC OK
#2 OK
IF R
MAIN
AC OK
ISOLATION
VALVE
FROZEN FROZEN
LDG GEAR IND OK
IF EBATTS
ON
NAV COMP #2 NO #1 NO
NAV RCVR #2 NO #1 NO
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EA - 24 May 30/02
Master Table Of Electrical Component Availability, ctd… GAC
AC BUSSES DC BUSSES
COMPONENT L MN
AC BUS
R MN
AC BUS
ESS AC
BUS
L MN
DC
BUS
R MN
DC
BUS
ESS DC
BUS
BATT
BUS
#1,
#2
NOSE STEER OK IF
ESS DC
OK
OK IF R
MAIN
DC OK
PERF COMP #1 NO #2 NO
PITCH/MACH
TRIM
#2 NO #1 NO
PITOT HEAT NO
RIGHT
NO
LEFT
NO
STBY
NO
RIGHT
NO
LEFT
NO
STBY
PRESSURIZATION
NO
AUTO
ZERO
OFF
RAD ALT #1 NO #2 NO
REVERSERS NO
SYM GEN #3 NO #2 NO #1 NO
TOE BRAKES OK IF
EBATTS
ON
TONE GEN NO
TRANSPONDER
TDR/CAD
#2 NO #1 OK
IF EBATTS
ON
VHF #2 NO #1 OK
IF EBATTS
ON
WIPERS NO
RIGHT
NO
LEFT
WX RADAR PILOTS
RDR
CONT
NO
COPILOTS
RDR
CONT
NO
X FLOW /
INTERTANK
FROZEN
YAW DAMPER #2 NO #1 NO
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EA - 25
Components Powered By The Emergency Batteries
OM 2A-24-30
Battery Function No. 1 Battery No. 2 Battery
Inboard Anti-skid
(HMAB)
Outboard Anti-skid
(HMAB)
No. 1 Clock No. 2 Clock
No. 1 Standby
DDRMI / DBDI
No. 2 Standby
DDRMI / DBDI
No. 1 COMM Standby Horizon
No. 1 COMM Cont. Left Fuel Qty. Ind.
Emergency Buses No. 1 Audio Right Fuel Qty. Ind.
No. 1 TDR / CAD Left Stby. Eng. Inst.
Stby. Mach/AS Ind. Right Stby. Eng. Inst.
Stby. Altimeter Cockpit Lights Cont.
Stby. Elec. Pwr. Pnl. Landing Gr. Pos. Lts.
BCS Channel 1 Flap / Horiz. Stab.
Position Indicator
Exterior Emergency
Lights (8 ea.)
Exterior Emergency
Lights (8 ea.)
No. 1 COMM No. 2 COMM
No. 1 TDR / CAD No. 1 TDR / CAD
Memory Keep Alive No. 1 NAV No. 2 NAV
No. 1 DME No. 2 DME
No. 1 ADF No. 2 ADF
NOTE FOR SN 1467 AND SUBS
Emergency Batteries No. 3 and No. 4 are added. The No. 3 Battery
powers the interior emergency lighting. The No. 4 Battery powers the
main entrance door emergency lighting (if main entrance door is
open).
END
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EA - 26 May 30/02
APU Starting on External DC Power AFM 3-04-10
CAUTION: ENSURE AC EXTERNAL POWER IS DISCONNECTED.
1. Battery 1 and 2 Switches...........................................................OFF
2. TRU Circuit Breaker ("AC RIGHT" Section Of PDB) ..............PULL
3. DC External Power.........................................................CONNECT
4. Electric Master Auxiliary Power.................................................. ON
5. Battery Voltage.................................... CHECK (ABOVE 4 VOLTS)
CAUTION: AIRPLANES WITHOUT ASC 54, THE BATTERIES
MUST BE DEEP CYCLED PRIOR TO FLIGHT IF BATTERY VOLTAGE
IS BELOW 4 VOLTS. IF BATTERY VOLTAGE IS BETWEEN 4 AND 20
VOLTS PRIOR TO APU START, BATTERIES MUST BE DEEP CYCLED
AT NEXT AVAILABLE MAINTENANCE FACILITY.
CAUTION: AIRPLANES WITH ASC 54 AND BATTERY VOLTAGE
BELOW 4 VOLTS, THE BATTERIES MUST BE DEEP CYCLED AT
NEXT AVAILABLE MAINTENANCE FACILITY AFTER USE OF THIS
PROCEDURE.
6. External DC ON Indicator Light.................................................. ON
7. BATT CHGR #1 and #2 Circuit Breakers (PDB)...............CLOSED
8. HP Fuel Cocks .......................................................................SHUT
9. APU Fire Warning ............................................................... CHECK
10. APU Air......................................................................................OFF
11. APU Master Switch .................................................................... ON
12. APU Oil Pressure Low Light...................ON (TEN [10] SECONDS)
13. Left Main Fuel Boost Pump........................................................ ON
14. APU Start Button....................................PRESS (MOMENTARILY)
15. APU Oil Pressure Low Light..................OUT (BEFORE 95% RPM)
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