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Boeing 737-600 - Subtask 76-11-02-420-005-F00; Subtask 76-11-02-410-001-F00; Subtask 76-11-02-420-006-F00; Subtask 76-11-02-040-007-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)
(c) Install the nut [100], the washer [101], the washer [102], the washer [103], and the
bolt [104].
NOTE: The bolt head is installed on the outboard side of the control link.
SUBTASK 76-11-02-420-005-F00
(9) Activate and adjust the stabilizer trim assembly as follows:
(a) Remove the temporary wire tie from the chain [39] and the sprocket [40].
(b) Adjust the stabilizer control chain (TASK 27-41-00-820-801).
SUBTASK 76-11-02-410-001-F00
(10) Connect the flap lever synchro assembly as follows:
(a) Put the link assembly [12] in the clevis for the flap lever synchro assembly.
(b) Install the nut [18] and the bolt [19].
SUBTASK 76-11-02-420-006-F00
(11) Connect the stabilizer trim indicator as follows:
(a) Put the link assembly [13] on the arm.
(b) Install the nut [16], the washer [15], the washer [14], and the bolt [17].
SUBTASK 76-11-02-040-007-F00
(12) Activate the speed brake lever as follows.
(a) Go into the access area below the forward flight compartment floor.
1) Remove the rig pin, part of rigging pin kit, SPL-1585, from the forward drum of the
speed brake mechanism.
2) Do this task: Speed Brake Control Lever Adjustment, TASK 27-62-00-820-801.
SUBTASK 76-11-02-420-007-F00
(13) Install the wheel assemblies for the stabilizer trim as follows:
(a) Install the right stabilizer trim wheel [7].
1) Install the right bolt [8] with the countersunk head.
2) Tighten the bolt to 150 in-lb (16.9 N·m) 170 in-lb (19.2 N·m).
3) Install the right bolt [8] and spacer.
4) Do a check of the run-on torque of the bolt.
5) Tighten the bolt to 150 in-lb (16.9 N·m) 160 in-lb (18.1 N·m) more than the run-on
torque.
(b) Do these steps to install the left stabilizer trim wheel [11]:
1) install the left stabilizer trim wheel [11].
a) FOR UNCLOCKED TRIM WHEEL AND SHAFT:
Set the crank of the left trim wheel 75 to 105 degrees from the setting of the
crank on the right trim wheel.
NOTE: This can be set in either direction.
2) Install the left bolt [8] with countersunk head.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-02
Page 429
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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