SUBTASK 53-05-02-410-164
(3) Close this access panel:
Number Name/Location
844 Aft Galley Service Door
NOTE: Re-attach scuff plates as required.
END OF TASK
TASK 53-05-02-210-837
207. INTERNAL - GENERAL VISUAL: PRESSURE DECK ATTACHMENTS TO REAR SPAR EXTENSION
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Right
B. Inspection
SUBTASK 53-05-02-210-037
(1) Do a General Visual inspection of the angle between the rear spar extension and the pressure
deck from the AFT or FWD side, including the bend radius.
NOTE: Either the AFT or FWD side inspection may be performed.
See Doc. D626A001-DTR, DTR check form 53-40-24-1 for alternative inspections.
END OF TASK
TASK 53-05-02-250-A98
208. EXTERNAL - SPECIAL DETAILED: AFT WHEEL WELL BULKHEAD, STA 727
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Right
141 Aft Cargo Compartment - Left
142 Aft Cargo Compartment - Right
143 Area Below Aft Cargo Compartment - Left
144 Area Below Aft Cargo Compartment - Right
193 Lower Wing-To-Body Fairing - Wheel Well
B. Inspection
SUBTASK 53-05-02-250-303
(1) Do a High Frequency Eddy Current inspection of the chord at frame 727 from stringers S-21L
to S-27L and stringers S-21R to S-27R.
See Doc. D626A001-DTR, DTR check form 53-40-16-1b 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 53-10-93.
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.28
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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