EasyManua.ls Logo

Boeing 737-600 - Task 53-05-02-211-833 - INTERNAL - DETAILED: WHEEL WELL FRAME, STA 685; Subtask 53-05-02-211-033; Task 53-05-02-250-861 - INTERNAL - SPECIAL DETAILED: WHEEL WELL FRAME, STA 685; Subtask 53-05-02-250-061

Boeing 737-600
2300 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
TASK 53-05-02-211-833
92. INTERNAL - DETAILED: WHEEL WELL FRAME, STA 685
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Right
241 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Left
242 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Right
B. Inspection
NOTE: Remove and/or displace passenger cabin sidewalls, sidewall air grilles, and insulation
blankets as required to perform the inspection.
SUBTASK 53-05-02-211-033
(1) Do a Detailed inspection of the frame inner chord from stringers S-13 to S-15.
See Doc. D626A001-DTR, DTR check form 53-40-21-2 for alternative inspections.
END OF TASK
TASK 53-05-02-250-861
93. INTERNAL - SPECIAL DETAILED: WHEEL WELL FRAME, STA 685
NOTE: This procedure is a scheduled maintenance task.
A. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station 727.00 - Right
241 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Left
242 Aft Passenger Compartment - Station 663.75 to Aft Pressure Bulkhead - Right
B. Inspection
SUBTASK 53-05-02-250-061
NOTE: Remove and/or displace passenger cabin sidewalls, sidewall air grilles, and insulation
blankets as required to perform the inspection.
(1) Do a High Frequency Eddy Current inspection of the frame inner chord flange and around
accessible fasteners common to the inner chord and stringer clips from stringers S-17 to S-14.
See Doc. D626A001-DTR, DTR check form 53-40-21-3 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 53-11-17.
END OF TASK
TASK 53-05-02-250-862
94. INTERNAL - SPECIAL DETAILED: WHEEL WELL FRAME AT STA 685
NOTE: This procedure is a scheduled maintenance task.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 252
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

Table of Contents

Related product manuals