1 THE DOOR SKIN CONTOUR (2 LOCATIONS)

(-) REFERS TO THE HANDLE INSIDE
A
THE DOOR SKIN CONTOUR
Exterior Handle Latch Adjustment Figure 502
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-13
 ALL  ú ú 01 Page 511 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 375-023
 (20)
 Apply the primer to the delamination surfaces of the shims.

 S 415-024

 (21)
 Install the cam (25) and the center shaft mechanism
 (Ref 52-11-13/401).

 NOTE: Do not install the support fitting.
____
 S 225-025
 (22)
 Do the step (2) to do a check for the correct shim thickness (16).

 S 415-026

 (23)
 Install the support fitting (17), control cam (18), shims (32) (if you removed), and stub shaft (31).

 S 825-027

 (24)
 If you adjusted the shims (22 or 26), do these steps to adjust the latch keeper on the external handle:

 (a)  
Close and latch the door.

 (b)  
With the external handles (2, 28,) in their positions, make sure the handle flushness is as shown in Fig. 502.

 (c)  
Do these steps to adjust the handle flushness, if it is necessary: 1) Extend the external handles. 2) Remove the fasteners that hold the latch keeper, the

 serrated plate, and the shim to the handle. 3) Remove and adjust the shim to get the correct flushness.
 NOTE: The shim thickness of the upper latch keeper (when
____ the handles are in the door closed position) will cause the incorrect fairing of the lower handle. Keep the shim thickness on the upper handle to a minimum (or remove the shim, if it is possible) . This will keep the lower handle in its correct position.
 4) Loosely assemble the latch keeper, the serrated plate, and shim with the bolts, nuts and washers. 5) Adjust the serrations to get a correct clearance between the latch and the latch keeper (Fig. 502). 6) Tighten the nuts.
 (d)
Do the steps (b) and (c) above with the door open.

 H.
Put the Airplane Back to Its Serviceable Condition

 (1)  
Install the entry door lining (Ref 52-11-02/401).

 S 415-030
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-13
 ALL  ú ú 04 Page 512 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 MAIN ENTRY DOOR HINGE FLAPS - REMOVAL/INSTALLATION
__________________________________________________
 1.  General_______
 A. This procedure contains these tasks:
 (1)
A task to remove the hinge flaps for the main entry door.

 (2)
A task to install the hinge flaps for the main entry door.

 TASK 52-11-14-004-001
 2.  Remove the Hinge Flap (Fig. 401)_____________________
 A. References
 (1)
IPC 52-11-03, 52-11-14

 B.
Access

 (1)  
Location Zone 211 Main Deck, Nose to First Door, LH 271 Main Deck, STA 2040 to STA 2360, LH

 (2)  
Access Panel 211AL Panel, Access - Door Maintenance (Door 1, LH) 271AL Panel, Access - Door Maintenance (Door 5, LH) 831L Door - No. 1 Main Entry, LH 835L Door - No. 5 Main Entry, LH

 C.
Procedure

 (1)  S 014-005Remove the maintenance access panel for the door.
 (2)  S 024-006Remove the hinge flap. (a) Remove the fasteners that attach the hinge flap to the hinge.
 NOTE:____ Keep the shims between the hinge and the hinge flap to use during installation.
 (b) (c)  Remove the hinge pin to disconnect the hinge.Remove the spring installation pin to remove the spring.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-14
 ALL  ú ú 03 Page 401 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 艙門 DOORS 1(111)