C. Access Panels
Number Name/Location
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
114AW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
D. Inspection
SUBTASK 53-05-02-010-015
(1) Open these access panels on the Left side:
Number Name/Location
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
Open these access panels on the Right side:
Number Name/Location
114AW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
NOTE: For Direction 1, removal of Drag Brace is required.
(a) Do this task: Nose Wheel Well Access Panels - Removal, TASK 53-14-01-020-801.
SUBTASK 53-05-02-211-010
(2) Do a Detailed inspection of the inboard and outboard drag brace fittings around the perimeter
of the bushings at Sta 262, BL 16, WL 189.3.
See Doc. D626A001-DTR, DTR check form 53-10-20-2 for alternative inspections.
SUBTASK 53-05-02-410-013
(3) Close these access panels on the Left side:
Number Name/Location
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
Close these access panels on the Right side:
Number Name/Location
114AW Forward Nose Wheel Well Panel
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 53-05-02-211-811
32. INTERNAL - DETAILED: NOSE LANDING GEAR TRUNNION SUPPORT FITTING
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)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-05-02
Page 215
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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