C. Inspection
SUBTASK 53-05-02-010-008
(1) Open this access panel:
Number Name/Location
822 Aft Cargo Door
SUBTASK 53-05-02-130-009
(2) Do an Ultrasonic inspection of the bearstrap for hidden damage under the stop backup fitting
at stringer S-24R at STA 794.4 and STA 847. (PSE 53-60-08-6).
See Doc D626A001-DTR, DTR check form 53-30-08-6 for alternative inspections.
SUBTASK 53-05-02-410-006
(3) Close this access panel:
Number Name/Location
822 Aft Cargo Door
END OF TASK
TASK 53-05-02-250-951
198. EXTERNAL - SPECIAL DETAILED: LONGITUDINAL LAP SPLICE
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
241 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Left
242 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Right
B. Inspection
SUBTASK 53-05-02-250-151
(1) Do a High Frequency Eddy Current inspection of the upper skin along the upper fastener row
at stringers S-4L and S-4R from STA 887 to STA 1016. (PSE 53-70-03-1).
See Doc. D626A001-DTR, DTR check form 53-10-03-1, 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 53-30-41.
END OF TASK
TASK 53-05-02-211-873
199. EXTERNAL - DETAILED: CROWN SKIN PANEL STA 887 TO STA 1016
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
241 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Left
242 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Right
B. Inspection
NOTE: Remove Dorsal Fin as required to perform the inspection.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.23
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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