SUBTASK 76-11-06-420-008-F00
(2) Install the rod assembly [20] to the interlock solenoid [31] or the solenoid [32] and latch
assembly:
(a) Put the rod assembly [20] on the interlock solenoid drive pin.
(b) Install the nut [21] and the washer [22].
1) Tighten the nut to 20 in-lb (2.26 N·m) – 25 in-lb (2.82 N·m).
(c) Set the rod end in its position on the interlock latch assembly.
(d) Install the bolt [26] and the washer [27].
SUBTASK 76-11-06-420-002-F00
(3) Connect the applicable wire bundles for the left interlock solenoid as follows:
(a) Make sure you route the bundle correctly.
ILF 301, 401, 405, 406, 409, 410, 412, 416, 424, 425, 427-429, 451, 501-504, 507-510, 512, 513 POST
SL 737-76-021
1) Route the bundle through the left aft lightening hole to prevent interference with the
left reverse thrust lever assembly.
NOTE: The bundle for the right interlock solenoid routes through the right aft
lightening hole.
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(b) Connect the three clamps.
(c) Remove the protective covers from the electrical connectors and receptacles.
(d) Connect the connector V155.
(e) Put the wire bundle in the protective cover.
SUBTASK 76-11-06-420-009-F00
(4) Connect the applicable wire bundles for the right interlock solenoid as follows:
(a) Make sure that you route the bundle correctly.
(b) Connect the four clamps.
(c) Remove the protective covers from the electrical connectors and receptacles.
(d) Connect the connector V156.
(e) Put the wire bundle in the protective cover.
SUBTASK 76-11-06-820-001-F00
(5) Adjust the latch assembly as follows:
(a) Set the distance between the roller and the brake assembly:
1) Loosen the top jamnut [23].
2) Loosen the bottom jamnut [25].
3) Turn the spinning rod [24] to set the distance between the roller and the brake
assembly to 0.0682 ±0.0300 in. (1.7323 ±0.7620 mm).
4) Tighten the top jamnut [23] and the bottom jamnut [25].
NOTE: Make sure that the spinning rod does not turn when you tighten the top
jamnut and the bottom jamnut.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-06
Page 414
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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