EXTERNAL POWER RECEPTACLE - INSPECTION/CHECK
1. General
A. This procedure has these tasks:
(1) External Power Receptacle - Internal Inspection.
(2) External Power Receptacle - External Inspection.
(3) External Power Receptacle Pin Inspection.
(4) External Power Receptacle Neutral Pin To Ground Continuity Check.
TASK 24-41-11-200-801
2. External Power Receptacle - Internal Inspection
(Figure 601 or Figure 602 or Figure 603)
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.
(2) The External Power Receptacle Inspection looks for visual wear such as cracks in the base
and corroded and pitted pins. This inspection also makes sure that the terminals are correctly
installed on the studs and that the torque is correct.
B. References
Reference Title
24-22-00-860-812 Remove Electrical Power (P/B 201)
C. Location Zones
Zone Area
116 Nose Landing Gear Wheel Well - Right
D. Access Panels
Number Name/Location
114AR External Power Receptacle Door
E. Prepare for Inspection
SUBTASK 24-41-11-860-006
(1) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
SUBTASK 24-41-11-010-004
(2) Open this access panel:
Number Name/Location
114AR External Power Receptacle Door
SUBTASK 24-41-11-010-005
(3) Remove External Power Plug from receptacle, if it is installed.
SUBTASK 24-41-11-930-002
WARNING
MAKE SURE YOU PUT A DO-NOT-OPERATE TAG ON THE EXTERNAL
POWER RECEPTACLE. INJURIES TO PERSONS CAN OCCUR IF YOU DO
NOT OBEY THIS INSTRUCTION.
(4) Attach a DO-NOT-OPERATE tag to the external power receptacle.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Page 601
D633A101-ILF Oct 15/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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