(Continued)
AMM Item Description AIPC Reference AIPC Effectivity
2 (cont.) 24-11-61-01A-015 ILF 101, 151, 156-199,
301, 304, 308, 310, 314,
315, 317-319, 323,
331-399, 402, 405, 410,
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,
803-813, 821, 822,
831-838, 841, 842, 851,
852, 854-858, 861-863,
871-874, 947, 948,
968-973, 980-999
E. Location Zones
Zone Area
410 Subzone - Engine 1
413 Engine 1 - Fan Cowl, Left
420 Subzone - Engine 2
423 Engine 2 - Fan Cowl, Left
F. Prepare for the Removal
SUBTASK 24-11-61-010-001
(1) Do this task: Open the Fan Cowl Panels, TASK 71-11-02-010-801-F00.
SUBTASK 24-11-61-010-002
(2) If the IDG is installed, do this task: Integrated Drive Generator (IDG) Removal,
TASK 24-11-11-000-801.
G. Procedure
SUBTASK 24-11-61-020-001
(1) Remove the QAD adapter per the steps that follow:
(a) Remove the twelve flathead screws [3] that attach the QAD adapter [1] to the gearbox
mount pad.
(b) Pull the QAD adapter [1] away from the pad.
NOTE: If the QAD adapter does not release easily from the pad, lightly hit it with a
rubber mallet, STD-3906.
(c) Remove the QAD adapter [1].
(d) Remove the gasket [2].
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-11-61
Page 402
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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