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Boeing 737-600 - Subtask 53-05-02-010-014; Subtask 53-05-02-211-009; Subtask 53-05-02-410-012; Task 53-05-02-211-810 - INTERNAL - DETAILED: NOSE LANDING GEAR SUPPORT FITTINGS

Boeing 737-600
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C. Access Panels
Number Name/Location
113BW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
D. Inspection
SUBTASK 53-05-02-010-014
(1) Open this access panel on the Left side:
Number Name/Location
113BW Forward Nose Wheel Well Panel
Open this access panel on the Right side:
Number Name/Location
114BW Forward Nose Wheel Well Panel
NOTE: Access through Left Aft Nose Wheel Well Panel.
Access through Right Aft Nose Wheel Well Panel.
(a) Do this task: Nose Wheel Well Access Panels - Removal, TASK 53-14-01-020-801.
SUBTASK 53-05-02-211-009
(2) Do a Detailed inspection of the Aft access cutout forward vertical beam at Sta 260, from WL
170 to WL 184.
See Doc. D626A001-DTR, DTR check form 53-10-19-4, for alternative inspections.
SUBTASK 53-05-02-410-012
(3) Close this access panel on the Left side:
Number Name/Location
113BW Forward Nose Wheel Well Panel
Close this access panel on the Right side:
Number Name/Location
114BW Forward Nose Wheel Well Panel
(a) Do this task: Nose Wheel Well Access Panels - Installation, TASK 53-14-01-420-801.
END OF TASK
TASK 53-05-02-211-810
31. INTERNAL - DETAILED: NOSE LANDING GEAR SUPPORT FITTINGS
NOTE: This procedure is a scheduled maintenance task.
A. References
Reference Title
53-14-01-020-801 Nose Wheel Well Access Panels - Removal (P/B 401)
53-14-01-420-801 Nose Wheel Well Access Panels - Installation (P/B 401)
B. Location Zones
Zone Area
113 Area Above and Outboard of Nose Landing Gear Wheel Well - Left
114 Area Above and Outboard of Nose Landing Gear Wheel Well - Right
115 Nose Landing Gear Wheel Well - Left
116 Nose Landing Gear Wheel Well - Right
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 214
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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