TASK 24-34-00-440-801
3. Standby Power System - Activation
(Figure 201)
A. General
(1) This procedure adds electrical power to the Standby Power System.
B. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
D. Procedure
SUBTASK 24-34-00-860-011
(1) Remove the safety tags and close these circuit breakers:
Battery Shield, J9
Row Col Number Name
A 4 C00142 BATTERY CHARGER
A 5 C01340 BATTERY BUS
ILF 493-500, 560-564, 567-569, 581, 583, 585, 588-590, 592-599, 601-603, 606, 607, 610-615, 620,
625-627, 671, 672, 691-699, 833-835, 838, 841, 842, 851, 852, 857, 858, 947, 948, 968-973, 980-999
SUBTASK 24-34-00-410-001
(2) Install the access cover on top of the J39 shield.
ILF ALL
SUBTASK 24-34-00-410-002
(3) Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-34-00
Page 204
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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