See Doc D626A001-DTR, DTR check form 53-80-01-3 for alternative inspections.
SUBTASK 53-05-02-410-028
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
END OF TASK
TASK 53-05-02-250-902
151. INTERNAL - SPECIAL DETAILED: BULKHEAD STA 1016
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
145 Aft Cargo Compartment Equipment Bay - Left
146 Aft Cargo Compartment Equipment Bay - Right
241 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Left
242 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
B. Inspection
NOTE: Remove necessary passenger cabin and aft cargo interiors as required to perform the
inspection.
SUBTASK 53-05-02-250-102
(1) Do a High Frequency Eddy Current inspection of the forward side of the pressure dome web
along the aft fastener row attaching the web to the pressure chord. Inspect at the edge of each
stiffener/clip and around the two fasteners on each side of the stiffener.
See Doc D626A001-DTR, DTR check form 53-80-01-4 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, Section 53-11-11.
END OF TASK
TASK 53-05-02-250-903
152. INTERNAL - SPECIAL DETAILED: BULKHEAD 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
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
B. Inspection
NOTE: Remove necessary passenger cabin interiors as required to perform the inspection.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 296
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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