ENGINE START BRAKE ASSEMBLY - REMOVAL/INSTALLATION
1. General
A. This procedure has two tasks:
(1) Engine Start Brake Assembly Removal
(2) Engine Start Brake Assembly Installation.
TASK 76-11-10-010-801-F00
2. Engine Start Brake Assembly Removal
(Figure 401, Figure 402, Figure 403 and Figure 404)
A. General
(1) This task provides the instructions on how to remove the engine start brake assembly from the
aisle control stand.
(2) The engine start brake assembly is referred to as the start brake assembly.
B. References
Reference Title
25-11-01-000-801 Captain's and First Officer's Seat Removal (P/B 401)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Prepare for the Removal
SUBTASK 76-11-10-040-001-F00
(1) Make sure that the left and right engine start switches are in OFF and install a
DO-NOT-OPERATE tag.
ILF 301, 304, 308, 310, 314, 315, 317-319, 323, 331-399, 533, 535, 537, 562; AIRPLANES WITH
AUTO-IGNITION
SUBTASK 76-11-10-860-006-F00
(2) Make sure the left and right engine start switches are in AUTO and install a
DO-NOT-OPERATE tag.
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
SUBTASK 76-11-10-860-007-F00
(3) For engine 1, open these circuit breakers and install the safety tags:
CAPT Electrical System Panel, P18-2
Row Col Number Name
A 1 C00458 ENGINE 1 IGNITION RIGHT
A 3 C00153 ENGINE 1 IGNITION LEFT
A 4 C01390 ENGINE 1 ALTN PWR CHAN B
A 5 C01314 ENGINE 1 ALTN PWR CHAN A
B 1 C01316 ENGINE 1 START LEVER CHAN A
B 2 C01317 ENGINE 1 START LEVER CHAN B
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-10
Page 401
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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