NOSE WHEEL WELL ACCESS PANELS - REMOVAL/INSTALLATION
1. General
A. This procedure contains these tasks:
(1) The removal of the Nose Wheel Well Access panels.
(2) The installation of the Nose Wheel Well Access panels.
TASK 53-14-01-020-801
2. Nose Wheel Well Access Panels - Removal
(Figure 401)
A. General
(1) This task gives the instructions to remove the nose wheel well access panels.
(2) The nose wheel well access panel is referred to as the access panel in this task.
B. References
Reference Title
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
C. Location Zones
Zone Area
115 Nose Landing Gear Wheel Well - Left
116 Nose Landing Gear Wheel Well - Right
D. Prepare for the Removal
SUBTASK 53-14-01-860-001
WARNING
OBEY THE PROCEDURE FOR THE INSTALLATION OF THE DOWNLOCK
PINS. IF YOU MOVE THE CONTROL LEVER FOR THE LANDING GEAR TO
THE UP POSITION, THE LANDING GEAR CAN RETRACT. THIS CAN CAUSE
INJURIES TO PERSONNEL, AND DAMAGE TO EQUIPMENT.
(1) Install the downlock pins for the main (Landing Gear Downlock Pins Installation,
TASK 32-00-01-480-801.)
E. Forward Side Access Panel Removal
SUBTASK 53-14-01-020-002
(1) Remove the forward access panels [15]:
(a) Remove the bolts [14].
(b) Remove the washers [2].
(c) Remove the O-ring seal washer [3].
SUBTASK 53-14-01-020-005
(2) Remove the forward access panel [15].
F. Aft Side Access Panel Removal
SUBTASK 53-14-01-020-006
(1) Remove the aft access panels [18]:
(a) Remove bolts [17].
(b) Remove the washers [2].
(c) Remove the O-ring seal washer [3].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-14-01
Page 401
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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