Boeing 737-600 - Subtask 24-41-11-210-004; Subtask 24-41-11-410-002; Subtask 24-41-11-410-003; Subtask 24-41-11-410-004

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
SUBTASK 24-41-11-210-004
(3) Inspect the External Power Receptacle from the inside of airplane as follows:
(a) Remove the dielectric separator.
(b) Look for discoloration of the receptacle terminals and electrical leads.
CAUTION
DO NOT INSTALL WASHERS BELOW THE ELECTRICAL LEAD
TERMINAL LUGS. THIS WILL CAUSE HEAT AND DAMAGE TO THE
TERMINAL STUDS.
(c) Make sure that the electrical leads are correctly installed onto receptacle.
(d) Look for loose nuts and bolts at the receptacle terminals. If you find loose nuts or bolts,
do these steps:
1) Tighten the bolts to 270 ±30 in-lb (30.5 ±3.4 N·m).
2) Tighten the nuts to 17.5 ±2.5 in-lb (1.98 ±0.29 N·m).
(e) Install the dielectric separator.
ILF ALL
SUBTASK 24-41-11-410-002
(4) Install the cover assembly [1] as follows:
(a) Put the cover assembly [1] in its position.
(b) Install the washers [3] and nuts [2].
(c) Tighten the nuts.
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
(d) Push the protective boot to the cover assembly [1] until it latches to the cover
assembly [1].
ILF ALL
SUBTASK 24-41-11-410-003
(5) Close the access panel on the forward right hand side of the nose gear wheel well.
SUBTASK 24-41-11-410-004
(6) Remove the DO-NOT-OPERATE tag from the external power receptacle, and close this access
panel:
Number Name/Location
114AR External Power Receptacle Door
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Page 603
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL