ILF 301, 304, 308, 310, 314, 315, 317-319, 323, 401, 402, 405, 406, 409, 410, 412, 416, 424, 425, 427-429, 451,
452, 501-504, 507-510, 512-516, 518-520, 523-528, 530-532, 536, 541, 542, 571, 703, 707, 708 (Continued)
F/O Electrical System Panel, P6-2
Row Col Number Name
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
B 9 C00440 FLIGHT CONTROL AUTO SPEED BRAKE
SUBTASK 76-11-10-040-004-F00
(6) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-3
Row Col Number Name
B 3 C00360 FUEL SPAR VALVE ENG 2
B 4 C00359 FUEL SPAR VALVE ENG 1
B 5 C00540 FUEL SPAR VALVE IND
SUBTASK 76-11-10-010-001-F00
(7) Do this task: Captain's and First Officer's Seat Removal, TASK 25-11-01-000-801.
E. Start Brake Assembly Removal
SUBTASK 76-11-10-010-002-F00
(1) Get access to the start brake assembly in the control stand as follows:
(a) Remove four screws [2] and the left upper side panel [1].
(b) Remove five screws [2] and the left lower side panel [5].
(c) Remove four screws [2] and the right upper side panel [3].
(d) Remove four screws [2] and the right lower side panel [4].
SUBTASK 76-11-10-020-001-F00
(2) For the start brake assembly (engine 1) [71], disconnect the electrical harness as follows:
(a) Remove the electrical connector [23] (D11286P).
(b) Remove the electrical connector [22] (D11288P).
(c) Disconnect the three clamps [21].
SUBTASK 76-11-10-020-002-F00
(3) For the start brake assembly (engine 2) [72], disconnect the electrical harness as follows:
(a) Remove the electrical connector [42] (D11292P).
(b) Remove the electrical connector [43] (D11290P).
(c) Disconnect the three clamps [41].
SUBTASK 76-11-10-020-003-F00
(4) Disconnect the applicable start lever from the start brake assembly as follows:
(a) Move the start lever to the IDLE position.
(b) Remove the nut [61], the washer [62], the washer [64] and the bolt [65].
SUBTASK 76-11-10-020-004-F00
(5) Remove the applicable start brake assembly as follows:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-10
Page 403
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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
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