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Boeing 737-600 - Subtask 76-11-06-010-005-F00; Subtask 76-11-06-010-006-F00; Subtask 76-11-06-410-004-F00; Subtask 76-11-06-440-004-F00

Boeing 737-600
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SUBTASK 76-11-06-010-005-F00
(3) Close this access panel:
Number Name/Location
114AW Forward Nose Wheel Well Panel
SUBTASK 76-11-06-010-006-F00
(4) Install the two access panels at the top of the wheel well.
SUBTASK 76-11-06-410-004-F00
(5) Close this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 76-11-06-440-004-F00
(6) Remove the DO-NOT-OPERATE tag from the ENGINE START switches.
SUBTASK 76-11-06-410-005-F00
(7) Do the activation procedure for the thrust reverser (TASK 78-31-00-440-803-F00).
SUBTASK 76-11-06-440-005-F00
(8) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
H. Reverse Thrust Interlock Solenoid Test
SUBTASK 76-11-06-710-004-F00
(1) Do this task: T/R LEVER INTLK (Interlock) TEST, TASK 73-21-00-700-805-F00.
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-06
Page 416
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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