25-21-25
ALL ú ú 01 Page 402 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
TASK 25-21-25-404-010
3. Sidewall Lining Panels Installation (Aft Entry and Service Doorways)___________________________________ (Fig. 401)
A. Access
(1) Location Zone
100 Upper Half of Fuselage
B. Install the Sidewall Lining Panels
S 424-011
(1)
Move the lining edges into the slot in the trim angle.
S 414-012
(2)
Install the seal retainer if it is applicable.
S 414-013
(3)
Install the rubber seal around the door opening.
S 414-014
(4)
Install the aid handle that is forward of the entry door if it is applicable.
S 414-015
(5)
Install the quarter-turn fasteners that attach the clearance cover to the forward structure of the door.
(6)
Install all the passenger equipment which you removed for access.
S 414-016
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-21-25
ALL ú ú 01 Page 403 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
SIDEWALL LINING PANELS (FORWARD ENTRY DOORWAY) - REMOVAL/INSTALLATION
_____________________________________________________________________
1. General_______
A. This procedure contains two tasks:
(1)
The removal of the Sidewall Lining Panels
(2)
The installation of the Sidewall Lining Panels
B. This procedure applies to the sidewall lining panel that attached to the structure around the opening of the forward entry door.
TASK 25-21-31-004-001
2. Sidewall Lining Panels Removal (Forward Entry Doorway) (Fig. 401)______________________________
A. Access
(1) Location Zone
105 Forward Entry Door
B. Procedure
S 014-002
(1)
Remove the passenger equipment if it is necessary to get access to the sidewall lining panel.
S 034-003
(2)
Remove the aid handle that is aft of the entry door.
S 014-004
(3)
Remove the hinge cover panels.
S 014-005
(4)
Remove the rubber seal from the retainer around the door opening.
S 014-006
(5)
Remove the screws that attach the trim angle and remove the forward and aft trim angles.
(6)
Remove the forward and aft kickplates.
S 024-008
(7)
Remove the quarter-turn fasteners that attach the panels forward of the door to the sidewall structure.
S 024-009
(8)
Remove the panel that is forward of the door.
S 034-007
(a) Move the panel aft and remove it.
S 024-010
(9) Remove the panel that is aft of the door.
(a) Pull the panel forward and inboard to be clear the from the windscreen attachment brackets.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-21-31
ALL ú ú 01 Page 401 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TRIM ANGLE
FWD
Sidewall Lining Panels Installation (Forward Entry Doorway)
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-21-31
ALL ú ú 01 Page 402 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(b) Move the panel forward and remove it.
TASK 25-21-31-404-011
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 EQUIPMENT/FURNISHINGS(49)
