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, 803, 808-811, 813, 854-856, 861-863, 871-874, 968-970, 972, 973 (Continued)
SUBTASK 53-05-02-410-082
(3) Close this access panel on the Left side:
Number Name/Location
833 Emergency Exit
Close this access panel on the Right side:
Number Name/Location
843 Emergency Exit
END OF TASK
TASK 53-05-02-250-872
104. INTERNAL - SPECIAL DETAILED: OVERWING EMERGENCY EXIT CUTOUT
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
231 Forward Passenger Compartment - Forward Entry Door to Sta 663.75 - Left
232 Forward Passenger Compartment - Forward Entry Door to Sta 663.75 - Right
B. Access Panels
Number Name/Location
833 Emergency Exit
843 Emergency Exit
C. Inspection
SUBTASK 53-05-02-010-140
(1) Open this access panel on the Left side:
Number Name/Location
833 Emergency Exit
Open this access panel on the Right side:
Number Name/Location
843 Emergency Exit
NOTE: Emergency Exit Door must be open to perform the inspection.
SUBTASK 53-05-02-250-072
(2) Do a High Frequency Eddy Current inspection on the edges of the doublers (on the upper
edge, for both upper corners of the cutout) at stringer S-11 from STA 616 to STA 639.
See Doc. D626A001-DTR, DTR check form 53-40-22-5 for alternative inspections.
NOTE: Doors with external doublers at the upper forward corner refer to DTR 53-40-22-20 for
area covered by the doubler.
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 53-30-37.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 261
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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