Boeing 737-600 - Subtask 24-41-11-860-012-001; Subtask 24-41-11-010-013-001; Subtask 24-41-11-020-006-001; Subtask 24-41-11-930-004-001

D. Consumable Materials
Reference Description Specification
A50419 Sealant - Pressure And
Environmental-Chromate, Type I, Class B-2
BMS5-95 Type I Class
B-2
E. Location Zones
Zone Area
116 Nose Landing Gear Wheel Well - Right
F. Access Panels
Number Name/Location
114AR External Power Receptacle Door
G. Prepare for Replacement
SUBTASK 24-41-11-860-012-001
(1) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
SUBTASK 24-41-11-010-013-001
(2) Open this access panel if it is closed:
Number Name/Location
114AR External Power Receptacle Door
SUBTASK 24-41-11-020-006-001
(3) Remove external power plug from the receptacle, if it is installed.
SUBTASK 24-41-11-930-004-001
(4) Attach a DO-NOT-OPERATE tag to the external power receptacle.
H. External Power Receptacle Pins Replacement
SUBTASK 24-41-11-020-014-001
(1) Do these steps to remove the shield [18] and doubler [19] from the receptacle [1]:
(a) Remove the nuts [17] and washers [16] that attach the shield [18] to the receptacle [1].
(b) Remove the shield [18].
1) Remove the sealant, A50419 from the shield [18] (if necessary).
(c) Remove the doubler [19].
1) Remove the sealant, A50419 from surface of the doubler [19].
SUBTASK 24-41-11-960-002-001
(2) Do these steps to replace the pins:
(a) For broken pins, use sharp tool to remove the broken external power receptacle pins and
use allen wrench, STD-7895 for large pins and hex wrench, STD-7012 for small pins to
install them.
(b) For worn out pins, try to slide the wear gage set, SPL-1625 over the external power
receptacle pins.
1) Make sure the gage does not slide over the pins. If the gage slides over the pins,
use allen wrench, STD-7895 for large pins and hex wrench, STD-7012 for small
pins to replace these pins.
(c) Tighten the large pins to 96.00 ±6.00 in-lb (10.85 ±0.68 N·m).
(d) Tighten the small pins to 24 ±4 in-lb (2.71 ±0.45 N·m).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 1
Page 412
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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