Boeing 737-600 - Page 418

ILF 491-495, 497, 559, 563, 564, 972; 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; ILF 588-590, 592, 980-999
POST SB 737-24-1203
(d) Put the doubler [19] in its position.
1) Apply sealant, A50419 to the surface of the doubler [19].
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
(e) Do these steps from out of the airplane:
1) Install the screw [15] from out of the airplane.
a) Tighten the screw [15] to 27.5 ±2.5 in-lb (3.11 ±0.29 N·m).
2) Put the shield [18] in its position.
3) Install the washers [16] and nuts [17].
a) Tighten the nuts [17] to 30 ±5 in-lb (3.4 ±0.6 N·m).
(f) Remove the excessive sealant, A00247.
(g) Apply sealant, A02315 to the edge of the receptacle [1] to make a fillet seal from inside
the airplane (TASK 51-31-00-390-804).
CAUTION
PUT AN IDENTIFIER ON THE WIRES ON EACH SIDE OF THE
ELECTRICAL CONNECTION BEFORE YOU DISCONNECT. IF YOU
CONNECT THEM AT AN INCORRECT LOCATION, DAMAGE TO THE
COMPONENTS WILL OCCUR.
CAUTION
DO NOT INSTALL WASHERS BELOW THE ELECTRICAL LEAD
TERMINAL LUGS. THIS WILL CAUSE HEAT AND DAMAGE TO THE
TERMINAL STUDS.
(h) Do these steps to install the electrical leads from in the airplane:
1) Put the electrical leads [13] in their positions.
2) Install the electrical leads [13] to the receptacle [1] with the washers [12], lock
washers [11] and bolts [10].
a) Tighten the bolts [10] to 270 ±30 in-lb (31 ±4 N·m).
3) Put the electrical leads [2] in their positions.
4) Install the electrical leads [2] to the receptacle [1] with the washers [3], lock
washers [4], and nuts [5].
a) Tighten the nuts [5] to 17.5 ±2.5 in-lb (1.98 ±0.29 N·m).
(i) Remove the identification tags from the electrical leads.
(j) Put the dielectric separator [6] in its position.
(k) Put the cover [9] in its position.
(l) Install the cover [9] to the receptacle [1] with the washers [7] and nuts [8].
1) Tighten the nuts [8] to 27.5 ±2.5 in-lb (3.11 ±0.29 N·m).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 1
Page 410
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