S 716-016
(3)
Operate the hatch from inside the airplane and make sure the operation is smooth:
(a)
Close the hatch and turn the interior handle counterclockwise 180 degrees to the latched position.
(b)
Open and move the hatch down and outboard.
(c)
Close and latch the hatch.
S 716-017
(4)
Operate the hatch from outside the airplane and make sure the operation is smooth:
(a)
Push the release trigger and extend the handle.
(b)
Turn the handle clockwise 180 degrees.
(c)
Open and move the hatch down and outboard.
(d)
Close and latch the hatch.
(5)
Install the acoustic pad on the hatch with velcro tape.
(6)
Close and latch the hatch.
S 416-018
S 866-019
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-21-00
ALL ú ú 01 Page 605 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
CREW COMPARTMENT OVERHEAD HATCH - REMOVAL/INSTALLATION
______________________________________________________
1. General_______
A. This procedure contains these tasks:
(1)
The removal of the crew compartment overhead hatch.
(2)
The installation of the crew compartment overhead hatch.
B.
The crew compartment overhead hatch will be called a hatch in these tasks.
TASK 52-21-01-004-001
2. Crew Compartment Overhead Hatch Removal (Fig. 401)_______________________________________
A. References
(1)
IPC 52-21-01 Fig. 1
B.
Access
(1)
Location Zone
221 Control Cabin, LH
(2)
Access Panel
839L Control Cabin Overhead Hatch
C.
Procedure
S 014-003
(1)
Remove the acoustic pad attached to the hatch internal panel.
S 864-016
(2)
Make sure the hatch is closed and latched.
S 034-004
(3)
Remove the bolt, washers, nut, and bushing from the two hinge brackets (View B). Put tags on the washers for the subsequent installation.
S 024-005
WARNING:_______MAKE SURE YOU HOLD THE HATCH. THE HATCH CAN FALL FROM THE OPENING WHEN IT IS UNLATCHED. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(4) Operate the inner handle to unlatch the hatch. Slowly move the hatch from the opening.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-21-01
ALL ú ú 01 Page 401 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
CREW COMPARTMENT OVERHEAD HATCH
INTERNAL PANEL
SEE A
INNER HANDLE
STOP FITTING HINGE
SEE C ARM WASHER
HINGE BRACKET NUT
WASHER
SHOULDERED
HINGE BRACKET HINGE ARM AND VELCRO TAPE SPACER BOLT WASHER (2 LOCATIONS)
SEE B (16 LOCATIONS) WASHER
WASHER (4 LOCATIONS)
0.03 INCH MAXIMUM
HINGE ARM AND HINGE BRACKET
CREW COMPARTMENT OVERHEAD HATCH B (INTERNAL VIEW) LAMINATED A SHIM
STOP FITTING
+0.02
0.10 INCH (STATION 360 ONLY) SERRATED
-0.06
KEEPER PLATE +0.04 FITTING
0.10 INCH (EXAMPLE, 3 LOCATIONS)
-0.06
STOP FITTING
C
Crew Compartment Overhead Hatch Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 艙門 DOORS 1(138)
