ILF ALL POST SB 737-CFM56-7B-80-0016
CAUTION
DO NOT TIGHTEN THE NUT TO MORE THAN THE MAXIMUM TORQUE.
DAMAGE TO THE PARTS CAN OCCUR.
(f) Tighten the nut on the clamp [7] to 115–125 pound-inches (13.0-14.1 Newton-meters), as
shown on the clamp.
ILF ALL
SUBTASK 80-11-01-420-005-F00
(7) Connect the starter duct [1] to the starter [9] as follows:
(a) Attach the starter duct [1] to the starter [9] with the coupling [2].
NOTE: Make sure that the key on the starter is aligned with the keyway on the duct.
(b) Tighten the nut on the coupling [2] to the torque given on the part.
(c) Lightly hit the outer surface of the coupling [2] with a rubber mallet, STD-3906.
(d) Tighten the nut on the coupling [2] again to the torque given on the part.
SUBTASK 80-11-01-610-001-F00
(8) If it has not done so, do this task: Starter Servicing (Oil Fill), TASK 80-11-01-610-801-F00.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 80-11-01-410-004-F00
(1) Do this task: Close the Fan Cowl Panels, TASK 71-11-02-410-801-F00.
SUBTASK 80-11-01-860-042-F00
(2) For Engine 1, remove the safety tag and close this circuit breaker:
CAPT Electrical System Panel, P18-2
Row Col Number Name
B 8 C01103 ENGINE 1 START VALVE
SUBTASK 80-11-01-860-043-F00
(3) For Engine 2, remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
C 4 C00154 ENGINE 2 START VALVE
I. Starter Installation Test
SUBTASK 80-11-01-700-002-F00
(1) Do the test(s) listed in the Power Plant Test Reference Table (TASK 71-00-00-800-811-F00).
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
80-11-01
Page 408
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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