ILF 151, 156-199, 401, 402, 405, 416, 452, 508-510, 523, 525-528, 536, 541, 542, 571-577, 671, 672, 686, 703,
707-710, 854-856, 861-863, 871-874, 968-970, 972, 973 (Continued)
Close this access panel on the Right side:
Number Name/Location
843 Emergency Exit
END OF TASK
ILF 101, 301, 304, 308, 310, 314, 315, 317-319, 323, 331-399, 406, 409, 410, 412, 424, 425, 427-429, 451, 491-504,
507, 512-516, 518-520, 524, 530-533, 535, 537, 552-557, 559-564, 567-569, 581, 583, 585, 588-590, 592-599,
601-603, 606, 607, 610-615, 620, 625-627, 691-699, 804-807, 812, 821, 822, 831-838, 841, 842, 851, 852, 857, 858,
947, 948, 971, 980-999
TASK 53-05-02-250-867
99. EXTERNAL - SPECIAL DETAILED: OVERWING EMERGENCY EXIT CUTOUT SKIN ASSEMBLY AND
FRAME OUTER CHORD
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
832 Left Forward Emergency Exit
842 Right Forward Emergency Exit
B. Access Panels
Number Name/Location
832 Emergency Exit
842 Emergency Exit
C. Inspection
SUBTASK 53-05-02-010-080
(1) Open this access panel on the Left side:
Number Name/Location
832 Emergency Exit
Open this access panel on the Right side:
Number Name/Location
842 Emergency Exit
SUBTASK 53-05-02-250-067
(2) Do a Low Frequency Eddy Current inspection of the doublers around the fasteners common to
the STA 578 cutout forward edge frame outer chord from stringers S-10 to S-13.
See Doc. D626A001-DTR, DTR check form 53-40-22-3 for alternative inspections.
The NDI method(s) necessary to accomplish the intent of this inspection is contained in the
737 Nondestructive Test Manual (D6-37239). The inspection procedures are contained in Part
6, Subject 53-11-16.
NOTE: This inspection must be work in conjunction with either fatigue task 53-682-01 or
53-682-03 to meet DTR requirements.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 256
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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