SUBTASK 53-05-02-130-007
(2) Do an Ultrasonic inspection of the top two fasteners in the outboard primary fittings common to
the STA 1088 bulkhead.
See Doc D626A001-DTR, DTR check form 53-80-06-1 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
4, Subject 53-80-01.
SUBTASK 53-05-02-410-005
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
END OF TASK
TASK 53-05-02-211-853
167. INTERNAL - DETAILED: VERTICAL FIN REAR SPAR ATTACHMENT FITTINGS
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
313 Stabilizer Torsion Box Compartment - Left
314 Stabilizer Torsion Box Compartment - Right
323 Vertical Fin - Front Spar To Rear Spar
B. Inspection
NOTE: Remove vertical fin including primary and fail-safe bolts.
SUBTASK 53-05-02-211-053
(1) Do a Detailed inspection of the four primary fitting lugs, from the inside of the lugs, at STA
1088.
See Doc D626A001-DTR, DTR check form 53-80-06-2 for alternative inspections.
END OF TASK
TASK 53-05-02-250-915
168. INTERNAL - SPECIAL DETAILED: BULKHEAD STA 1156
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
313 Stabilizer Torsion Box Compartment - Left
314 Stabilizer Torsion Box Compartment - Right
317 Tail Cone Compartment - Left
318 Tail Cone Compartment - Right
B. Access Panels
Number Name/Location
318BR Tailcone Access Door
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.7
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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