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Boeing 737-600 - Subtask 76-11-06-420-004-F00; Subtask 76-11-06-420-005-F00; Subtask 76-11-06-020-008-F00; Subtask 76-11-06-420-007-F00

Boeing 737-600
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SUBTASK 76-11-06-420-004-F00
(6) Attach the forward autothrottle assembly to the floor frame as follows
(TASK 70-20-02-400-801-F00):
(a) Move the autothrottle assembly up into its location.
(b) Install the right bolt [11] and the right washer [12].
(c) Install the left bolt [13] and the left washer [14].
(d) Remove all of the wood blocks.
SUBTASK 76-11-06-420-005-F00
(7) Attach the aft autothrottle assembly to the floor frame as follows
(TASK 70-20-02-400-801-F00):
(a) Tighten the right bolt [9].
(b) Tighten the left bolt [10].
SUBTASK 76-11-06-020-008-F00
(8) Connect the aft two cable guards to the nose wheel well housing as follow
(TASK 70-20-02-400-801-F00):
(a) Install the four bolts [8].
(b) Install the four nuts [6] and the washers [7].
SUBTASK 76-11-06-420-007-F00
(9) Attach the flap control cables.
(a) Connect the WFA and WFB cables (TASK 20-10-91-400-801).
SUBTASK 76-11-06-420-006-F00
(10) Connect the two thrust lever connecting rods [5] to the autothrottle clutch pack as follow:
(a) Set the applicable connecting rod to the autothrottle clutch pack.
(b) Install the nuts [3], the washers [2], and the bolts [1].
NOTE: Make sure you put the head of the bolt on the inboard side of the applicable
clutch pack.
(c) Install new cotter pins [4].
G. Put the Airplane Back to its Usual Condition
SUBTASK 76-11-06-710-003-F00
(1) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-2
Row Col Number Name
B 6 C01412 ENGINE 1 THRUST REVERSER INTLK
F/O Electrical System Panel, P6-2
Row Col Number Name
C 6 C01413 ENGINE 2 THRUST REVERSER INTLK
SUBTASK 76-11-06-710-005-F00
(2) Do this task: Thrust Lever Angle Resolver Adjustment, TASK 76-11-05-820-801-F00.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-06
Page 415
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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