EXTERNAL POWER RECEPTACLE - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) External Power Receptacle Removal
(2) External Power Receptacle Installation
(3) External Power Receptacle Pins Replacement
TASK 24-41-11-000-802-001
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. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Receptacle 24-41-11-01-135 ILF 401, 406, 409
24-41-11-01B-080 ILF 405, 410, 416, 424,
425, 427-429, 501-504,
512, 513
24-41-11-01B-275 ILF 101, 151, 156-199,
301, 304, 308, 310, 314,
315, 317-319, 323,
331-399, 402, 451, 452,
491-500, 507-510,
514-516, 518-520,
523-528, 530-533,
535-537, 541, 542,
552-557, 559-564,
567-569, 571-577, 581,
583, 585, 671, 672, 703,
707-710, 804-807, 812,
821, 822, 831, 832, 836,
837, 841, 842, 851, 852,
854-858, 861-863,
871-874, 947, 948,
968-973
24-41-11-02-155 ILF 412
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 1
Page 401
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 491-495, 497, 559, 563, 564, 588-590, 592, 972, 980-999; ILF 101, 151,
156-199, 301, 304, 308, 310, 314, 315, 317-319, 323, 331-399, 401, 402, 405, 406,
409, 410, 412, 416, 424, 425, 427-429, 451, 452, 496, 498-504, 507-510, 512-516,
518-520, 523-528, 530-533, 535-537, 541, 542, 552-557, 560-562, 567-569,
571-577, 581, 583, 585, 671, 672, 703, 707-710, 803-813, 821, 822, 831, 832, 836,
837, 841, 842, 851, 852, 854-858, 861-863, 871-874, 947, 948, 968-971, 973 POST
SB 737-24-1198
To Next Page
Loading...
