B. Inspection
NOTE: Remove necessary passenger cabin interiors as required to perform the inspection.
SUBTASK 53-05-02-250-110
(1) Do a Low Frequency Eddy Current inspection on the forward side of the pressure dome web
around the fasteners common to the doubler, Y-Chord and the tear strap between stringers S-1
and S-3.
See Doc D626A001-DTR, DTR check form 53-80-01-13 for alternative inspections.
END OF TASK
TASK 53-05-02-211-888
161. INTERNAL - DETAILED: BULKHEAD STA 1016
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
B. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
C. Inspection
SUBTASK 53-05-02-010-071
(1) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 53-05-02-211-088
(2) Do a Detailed inspection of the aft side of STA 1016 bulkhead web for oil cans.
NOTE: Refer to Structural Repair Manual, Section 53-80-08, for definition of oil can.
No DTR form available for PSE 53-80-01-14.
SUBTASK 53-05-02-410-069
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
END OF TASK
TASK 53-05-02-211-852
162. INTERNAL - DETAILED: VERTICAL FIN FRONT SPAR FITTING BULKHEAD ATTACHMENT - 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
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.3
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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