C. Inspection
SUBTASK 53-05-02-010-107
(1) Open this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 53-05-02-250-115
(2) Do a High Frequency Eddy Current inspection on the edge of the outer chord and the web
above and below the stab pivot line.
See Doc D626A001-DTR, DTR check form 53-80-07-1 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 53-10-85.
SUBTASK 53-05-02-410-105
(3) Close this access panel:
Number Name/Location
318BR Tailcone Access Door
END OF TASK
TASK 53-05-02-250-916
169. INTERNAL - SPECIAL DETAILED: INTEGRATED 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
C. Inspection
SUBTASK 53-05-02-010-108
(1) Open this access panel:
Number Name/Location
318BR Tailcone Access Door
NOTE: Enter aircraft through the tail cone access panel.
SUBTASK 53-05-02-250-116
(2) Do a High Frequency Eddy Current inspection of the web inboard along the failsafe strap from
the top of the stabilizer attach fitting down 16 inches vertically.
See Doc D626A001-DTR, DTR check form 53-80-07-2 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 53-11-33.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.8
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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