(Continued)
AMM Item Description AIPC Reference AIPC Effectivity
32 Solenoid 76-11-06-01-065 ILF 101, 151, 156-199,
301, 304, 308, 310, 314,
315, 317-319, 323,
331-399, 401, 402, 406,
409, 410, 412, 416, 424,
425, 427-429, 451, 452,
491-504, 507-510,
512-516, 518-520,
523-528, 530-533,
535-537, 541, 542,
552-557, 559-564,
567-569, 571-577, 581,
583, 585, 588-590,
592-599, 601-603, 606,
607, 610-615, 620,
625-627, 671, 672, 686,
691-699, 703, 707-710,
804-807, 812, 821, 822,
831-838, 841, 842, 851,
852, 854-858, 861-863,
871-874, 947, 948,
968-973, 980-999
D. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
113 Area Above and Outboard of Nose Landing Gear Wheel Well - Left
114 Area Above and Outboard of Nose Landing Gear Wheel Well - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
E. Access Panels
Number Name/Location
112A Forward Access Door
114AW Forward Nose Wheel Well Panel
F. Reverse Thrust Interlock Solenoid Installation
SUBTASK 76-11-06-420-001-F00
(1) Install the applicable interlock solenoid [32] or the interlock solenoid [31] as follows
(Figure 402, view C):
(a) Install the spacer [30].
(b) Put the applicable interlock solenoid [32] or the interlock solenoid [31] in its position as
follows:
1) Install the interlock solenoid [32] on the left side.
2) Install the interlock solenoid [31] on the right side.
(c) Install the two nuts [28] and the two washers [29].
1) Tighten the nuts to 20 in-lb (2.26 N·m) – 25 in-lb (2.82 N·m).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-06
Page 413
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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