SUBTASK 53-05-02-410-106
(3) Close this access panel:
Number Name/Location
318BR Tailcone Access Door
END OF TASK
TASK 53-05-02-250-917
170. INTERNAL - SPECIAL DETAILED: HORIZONTAL STABILIZER PIVOT FITTING
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
B. Inspection
NOTE: Remove sliding seals for access.
SUBTASK 53-05-02-250-117
(1) Do a High Frequency Eddy Current inspection of the pivot fitting beams around the pivot pins
at the STA 1156 hinge beam.
See Doc D626A001-DTR, DTR check form 53-80-08-1 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 53-10-86.
END OF TASK
TASK 53-05-02-230-801
171. INTERNAL - SPECIAL DETAILED: HORIZONTAL STABILIZER PIVOT PINS
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
B. Inspection
NOTE: Removal and separation of pivot pins is required to perform the inspection.
SUBTASK 53-05-02-230-001
(1) Do a Dye Penetrant of both the inner and outer pivot pins at STA 1156.
See Doc D626A001-DTR, DTR check form 53-80-08-2 for alternative inspections.
END OF TASK
TASK 53-05-02-211-854
172. EXTERNAL - DETAILED: SECTION 48 SKIN PANELS, STA 1088 TO STA 1156
NOTE: This procedure is a scheduled maintenance task.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.9
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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