EXTERNAL POWER RECEPTACLE - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) External Power Receptacle Removal
(2) External Power Receptacle Installation
TASK 24-41-11-000-803-002
2. External Power Receptacle Removal
(Figure 401)
A. General
(1) The External Power Receptacle is located on the lower right hand side of the airplane. It is
installed forward of the nose gear wheel well.
B. References
Reference Title
24-22-00-860-812 Remove Electrical Power (P/B 201)
C. Consumable Materials
Reference Description Specification
A50419 Sealant - Pressure And
Environmental-Chromate, Type I, Class B-2
BMS5-95 Type I Class
B-2
D. Location Zones
Zone Area
116 Nose Landing Gear Wheel Well - Right
E. Access Panels
Number Name/Location
114AR External Power Receptacle Door
F. Prepare for the Removal
SUBTASK 24-41-11-860-017-002
(1) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
SUBTASK 24-41-11-010-016-002
(2) Open this access panel if it is closed:
Number Name/Location
114AR External Power Receptacle Door
SUBTASK 24-41-11-010-017-002
(3) Remove External Power Plug from the receptacle, if it is installed.
SUBTASK 24-41-11-930-006-002
WARNING
PUT A DO-NOT-OPERATE TAG ON THE EXTERNAL POWER RECEPTACLE.
IF YOU DO NOT OBEY THIS INSTRUCTION, INJURIES TO PERSONS CAN
OCCUR.
(4) Attach a DO-NOT-OPERATE tag to the external power receptacle.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 2
Page 401
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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