(Continued)
AMM Item Description AIPC Reference AIPC Effectivity
12 Screw 30-11-11-02-010 ILF 101, 151, 156-199,
301, 304, 308, 310, 314,
315, 317-319, 323,
331-399, 401, 402, 405,
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
F. Location Zones
Zone Area
520 Subzone - Left Wing: Leading Edge, Fwd of Front Spar, Outboard of Strut and
Nacelle Gap Cover Area
620 Subzone - Right Wing: Leading Edge, Forward of Front Spar, Outboard of Nacelle
Strut
G. Access Panels
Number Name/Location
521AB Outboard Leading Edge Blowout Door - Slat Station 20.04
521AT Outbd Leading Edge - Gap Cover Access
621AB Outboard Leading Edge Blowout Door - Slat Station 20.04
621AT Outbd Leading Edge - Gap Cover Access
H. Prepare for the Installation
SUBTASK 30-11-11-040-002
WARNING
DO THE DEACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS.
THE SLATS RETRACT QUICKLY. THIS CAN CAUSE INJURIES TO
PERSONNEL OR DAMAGE TO EQUIPMENT.
(1) Make sure the leading edge slats are deactivated (TASK 27-81-00-040-801).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
30-11-11
Page 408
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
To Next Page
Loading...
