SUBTASK 24-41-11-010-018-002
(5) Open access panel on forward right hand side of nose gear wheel well, to get access to the
back of the receptacle.
G. External Power Receptacle Removal
SUBTASK 24-41-11-020-010-002
CAUTION
PUT AN IDENTIFIER ON THE WIRES ON EACH SIDE OF THE ELECTRICAL
CONNECTION BEFORE YOU DISCONNECT. IF YOU CONNECT THEM AT AN
INCORRECT LOCATION, DAMAGE TO THE COMPONENTS WILL OCCUR.
CAUTION
DO NOT INSTALL WASHERS BELOW THE ELECTRICAL LEAD TERMINAL
LUGS. THIS WILL CAUSE HEAT AND DAMAGE TO THE TERMINAL STUDS.
(1) Do these steps to remove the electrical leads from the receptacle [1]:
(a) Remove the nuts [11] and washers [12].
(b) Remove the cover assembly [10].
(c) Remove the washers [13].
(d) Attach an identification tag to each electrical lead.
(e) Remove the nuts [6], lockwashers [5], and washers [4].
(f) Remove the nuts [9], lockwashers [8], and washers [7].
(g) Remove the electrical leads from the studs.
SUBTASK 24-41-11-020-011-002
(2) Do these steps to remove the receptacle [1]:
NOTE: This step works best with two people, one outside the airplane and one inside the
wheel well access. However if only one person is available, you can put tape over the
bolts to prevent them from falling out when the nuts are removed.
(a) Remove the nuts [14], nuts [15], and washers [16].
(b) Remove the bolts [2] and washers [3].
(c) Remove the shield [17].
1) Remove the sealant, A50419 from the shield [17] (if necessary).
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 2
Page 402
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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