(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 Installation
SUBTASK 24-11-61-210-001
(1) Visually examine the mating surfaces of the QAD adapter and the gearbox mounting pad.
NOTE: The surfaces must be smooth and clean.
G. Procedure
SUBTASK 24-11-61-420-001
(1) Install the QAD adapter [1] per the steps that follow:
CAUTION
YOU MUST NOT LET GREASE GET INTO THE DOWEL PIN HOLES AND
BOLT HOLES. IF GREASE GETS INTO THESE HOLES DAMAGE TO THE
GEARBOX CAN OCCUR DUE TO PRESSURE BUILDUP WHEN THE
BOLTS ARE INSTALLED AND TIGHTENED.
(a) Apply a light coat of silicone compound, D00254, to the QAD flange and gearbox pad
where they contact the gasket [2].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-11-61
Page 406
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
To Next Page
Loading...
