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Boeing 737-600 - Subtask 53-05-02-211-054; Task 53-05-02-211-862 - EXTERNAL - DETAILED: CROWN SKIN PANEL STA 259.5 TO STA 360; Subtask 53-05-02-211-062; Task 53-05-02-250-931 - INTERNAL - SPECIAL DETAILED: FWD GALLEY DOOR CUTOUT

Boeing 737-600
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A. Location Zones
Zone Area
313 Stabilizer Torsion Box Compartment - Left
314 Stabilizer Torsion Box Compartment - Right
B. Inspection
SUBTASK 53-05-02-211-054
(1) Do a Detailed inspection of the skin panels around the STA 1138 cutout.
See Doc D626A001-DTR, DTR check form 53-80-10-1 for alternative inspections.
END OF TASK
TASK 53-05-02-211-862
173. EXTERNAL - DETAILED: CROWN SKIN PANEL STA 259.5 TO STA 360
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
221 Passenger Compartment - Aft of Control Compartment to Forward Entry Door - Left
222 Passenger Compartment - Aft of Control Compartment to Forward Entry Door -
Right
B. Inspection
SUBTASK 53-05-02-211-062
(1) Do a detailed inspection of the skin around all of the fastener locations from stringer S-10L to
S-10R, from Sta 259.5 to Sta 360, except at the lap splices and antennas. (53-10-08-1).
See Doc D626A001-DTR, DTR check form 53-30-01-2 for alternative inspections.
END OF TASK
TASK 53-05-02-250-931
174. INTERNAL - SPECIAL DETAILED: FWD GALLEY DOOR CUTOUT
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
118 Electrical and Electronics Compartment - Right
222 Passenger Compartment - Aft of Control Compartment to Forward Entry Door -
Right
B. Inspection
NOTE: Removal of scuff plate is required to perform the inspection.
SUBTASK 53-05-02-250-131
(1) Do a High Frequency Eddy Current inspection of the skin around the fastener holes and along
the edge of the cutout hidden by the scuff plates from STA 303 to STA 350. (53-10-15–4).
See Doc. D626A001-DTR, DTR check form 53-10-14-12 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 53-30-43.
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 298.10
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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