E. Procedure
SUBTASK 24-21-52-420-002
(1) Do these steps to install the module [1]:
(a) Put the module [1] carefully into position in the P5 overhead panel.
(b) Tighten the quarter turn fasteners on the module [1].
(c) Remove the protective covers from the electrical connectors.
(d) Examine the electrical connectors for bent or broken pins, dirt and damage.
1) Clean or repair the electrical connectors if it is necessary.
(e) Connect the electrical connectors to the module [1].
(f) Push the P5 overhead panel up to the closed position and latch it.
F. Installation Test of the Generator Drive and Standby Power Module
SUBTASK 24-21-52-710-001
(1) Do these tasks: Number 1 IDG - Operational Test, TASK 24-11-00-700-802 and Operational
Test For Number 2 IDG, TASK 24-11-00-700-803.
SUBTASK 24-21-52-710-004
(2) Do this task: The Operational Test of the Standby Power System, TASK 24-34-00-710-801 or
The Operational Test of the Standby Power System, TASK 24-34-00-710-802.
G. Put the Airplane Back to its Usual Condition
SUBTASK 24-21-52-710-002
(1) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-21-52
Page 405
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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