(g) Install the washers [12] and nuts [11].
1) Tighten the nuts [11].
SUBTASK 24-41-11-420-006-002
(3) Close the access panel on the forward right hand side of the nose gear wheel well.
G. External Power Receptacle Installation Test
SUBTASK 24-41-11-860-018-002
(1) Do this task: Supply External Power, TASK 24-22-00-860-813.
SUBTASK 24-41-11-860-019-002
(2) Make sure external power comes on line and operates correctly.
H. Cabin Pressure Leak Test
SUBTASK 24-41-11-700-003-002
(1) Do this task to make sure that there are no air leaks: Cabin Pressure Leak Test,
TASK 05-51-91-790-801.
I. Put the Airplane Back to Its Usual Condition
SUBTASK 24-41-11-860-020-002
(1) If electrical power is not necessary, do this task: Remove Electrical Power,
TASK 24-22-00-860-812.
SUBTASK 24-41-11-410-011-002
(2) Close this access panel:
Number Name/Location
114AR External Power Receptacle Door
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 2
Page 408
D633A101-ILF Oct 15/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 593-599, 601-603, 606, 607, 610-615, 620,
625-627, 691-699, 833-835, 838
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