Boeing 737-600 - Subtask 76-11-02-860-011-F00; Subtask 76-11-02-040-006-F00; Subtask 76-11-02-010-001-F00; Subtask 76-11-02-010-002-F00

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 76-11-02-860-011-F00
(6) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-1
Row Col Number Name
E 1 C00721 AUTOTHROTTLE DC 1
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
E 3 C01141 AUTOTHROTTLE DC 2
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 76-11-02-040-006-F00
(7) Deactivate the speed brakes and control lever as follows:
(a) Move the speed brake lever to the DOWN position.
(b) Go to the forward bay below the flight compartment.
(c) Install a rig pin S/B-1 from the rigging pin kit, SPL-1585 into the forward drum of the
speed brake mechanism.
SUBTASK 76-11-02-010-001-F00
(8) Do this task: Captain's and First Officer's Seat Removal, TASK 25-11-01-000-801.
SUBTASK 76-11-02-010-002-F00
(9) Put a mat on the aft electronics panel P8.
NOTE: This will prevent damage to the switches and glass surfaces of the indicators and
displays.
SUBTASK 76-11-02-020-015-F00
(10) Do this task: Control Stand Cover and Stop Removal, TASK 76-11-03-400-803-F00.
G. Start Lever Removal
SUBTASK 76-11-02-010-008-F00
(1) Remove the first officers stabilizer trim lightplate and the flap indicator lever lightplate
(TASK 76-11-03-000-801-F00).
SUBTASK 76-11-02-010-009-F00
(2) Remove these retainers and seals (TASK 76-11-03-400-801-F00):
(a) The right seal retainer and the right seal
(b) The center seal retainer and the center seal
(c) The left seal retainer and the left seal.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 404
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL