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Boeing 737-600 - Subtask 76-11-02-010-010-F00; Subtask 76-11-02-010-011-F00; Subtask 76-11-02-010-012-F00; Subtask 76-11-02-020-014-F00

Boeing 737-600
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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, 491-504, 507-510, 512-516, 518-520, 523-528, 530-533, 535-537, 541, 542,
552-557, 559-564, 567-569, 571-577, 581, 583, 585, 588-590, 592-599, 601-603, 606, 607, 610-615, 620, 671, 672,
686, 691-699, 703, 707-710, 803-813, 821, 822, 831-834, 836, 837, 841, 842, 851, 852, 854-858, 861-863, 871-874,
947, 948, 968-973, 980-999 (Continued)
SUBTASK 76-11-02-010-010-F00
(3) Remove the stabilizer trim horn cutout switch knob [6].
SUBTASK 76-11-02-010-011-F00
(4) Remove forward thrust stop and the aft thrust stop (TASK 76-11-03-400-803-F00):
SUBTASK 76-11-02-010-012-F00
(5) Move the right side cover assembly forward and carefully lay it on the front of the stand.
SUBTASK 76-11-02-020-014-F00
(6) Remove the center cover assembly(TASK 76-11-03-400-803-F00):
SUBTASK 76-11-02-010-005-F00
(7) Get access to the start levers in the control stand as follows :
(a) Remove the bolt [8] and the right stabilizer trim wheel [7].
NOTE: Keep the left stabilizer trim wheel attached so you can turn the assembled levers
during removal.
(b) Remove the spacer.
NOTE: The spacer is not installed with the countersunk head bolt.
(c) Remove the four screws [2] and the left upper side panel [1].
(d) Remove the five screws [2] and the left lower side panel [5].
(e) Remove the four screws [2] and the right upper side panel [3].
(f) Remove the four screws [2] and the right lower side panel [4].
(g) Remove the four screws [9].
(h) Apply masking tape, G50314 to prevent damage to the surface of the stabilizer trim
switch panel [10].
(i) Move the stabilizer trim switch panel [10] from the control stand to the mat.
SUBTASK 76-11-02-020-001-F00
(8) Disconnect the flap indicator assembly on the right side of the control stand as follows:
(a) Remove the nut [16], the washer [14], the washer [15], and the bolt [17] from the lower
end of the link assembly [13].
(b) Use a temporary wire tie to safety the link assembly to the control stand.
SUBTASK 76-11-02-020-002-F00
(9) Disconnect the flap lever position synchro assembly on the right side of the control stand as
follows:
(a) Remove the nut [18] and the bolt [19] from the lower end of the link assembly [12].
(b) Use a wire tie to temporarily safety the link assembly to the control stand.
SUBTASK 76-11-02-020-003-F00
(10) Disconnect the stabilizer trim controls as follows:
(a) Turn the left trim wheel until you find the link in the trim chain.
NOTE: This will help if it becomes necessary to disconnect the chain during installation.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 405
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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