C. Inspection
SUBTASK 53-05-02-010-106
(1) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
NOTE: Remove access panel as required. Remove/disconnect the jackscrew from the fitting
and move aside for access to the lugs.
SUBTASK 53-05-02-250-114
(2) Do a High Frequency Eddy Current inspection of both primary jackscrew fitting lugs on both
sides around the bushing at the STA 1088 bulkhead.
See Doc D626A001-DTR, DTR check form 53-80-05-1 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 53-10-95.
SUBTASK 53-05-02-410-104
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
END OF TASK
TASK 53-05-02-130-807
166. INTERNAL - SPECIAL 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. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
C. Inspection
SUBTASK 53-05-02-010-007
(1) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
NOTE: Access fittings inside the tailcone on the forward and aft side of the Sta 1088
Bulkhead. The top of the fittings are sandwiched between the splice angles and the
bulkhead.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.6
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
To Next Page
Loading...
