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Boeing 737-600 - Subtask 76-11-01-010-006-F00; Subtask 76-11-01-420-008-F00; Subtask 76-11-01-200-001-F00; Subtask 76-11-01-410-003-F00

Boeing 737-600
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SUBTASK 76-11-01-010-006-F00
(16) Install the access covers on to the control stand as follows.
(a) Install the left upper side panel [1] with the four screws [2].
(b) Install the left lower side panel [5] with the five screws [2].
(c) Install the right upper side panel [3].with the four screws [2].
(d) Install the right lower side panel [4] with the four screws [2].
SUBTASK 76-11-01-420-008-F00
(17) 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 countersunk head.
2) Tighten the bolt to 150 in-lb (16.9 N·m) 170 in-lb (19.2 N·m).
3) Install the 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) Install the left stabilizer trim wheel [11] as follows:
1) Put the left stabilizer trim wheel [11] in its position.
a) FOR UNLOCKED TRIM WHEEL AND SHAFT; Set the crank of the left trim
wheel 75 to 105 degrees away 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.
3) Tighten the bolt to 150 in-lb (16.9 N·m) 170 in-lb (19.2 N·m).
4) Install the left bolt [8] and spacer.
5) Do a check of the run-on torque of the bolt.
6) Tighten the bolt to 150 in-lb (16.9 N·m) 160 in-lb (18.1 N·m) more than the run-on
torque.
SUBTASK 76-11-01-200-001-F00
(18) Do a visual check of the assembly as follows:
(a) Move each control through its usual range.
(b) Make sure that the electrical bundles do not touch parts.
SUBTASK 76-11-01-410-003-F00
(19) Install the stabilizer trim switch panel [10] for the trim stabilizer as follows:
(a) Put the stabilizer trim switch panel [10] on the control stand.
(b) Install the four screws [9].
SUBTASK 76-11-01-700-001-F00
(20) Do this task: Thrust Lever Angle Resolver Adjustment, TASK 76-11-05-820-801-F00.
SUBTASK 76-11-01-410-004-F00
(21) Install these covers and stops (TASK 76-11-03-400-804-F00):
(a) The right cover and the right side cover assembly.
(b) The center cover.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-01
Page 431
D633A101-ILF Jun 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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