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 NOTE: If entry door impacts any object outside airplane during normal
____ door operation, immediately stop door operation and refer to 52-11-00, Inspection/Check, for quick check procedure to verify that door will still function properly.
 (1)  The door (No. 1 or 5) is opened manually from inside the airplane by rotating the interior handle 180 degrees to move the door inward to the cocked position, then manually pushing the door outward to the full open position.
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 52-11-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
UPPER GATE
BODY TORQUE 
TUBE 
SEE  A 
FWD 
DOOR 1 
BODY TORQUE
TUBE 
SEE  B 

DOOR 5
Main Entry Door Body Torque Tube Figure 3 (Sheet 1)
C72013
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

UPPER LINK
UPPER HINGE ARM TELESCOPIC SLEEVE UPPER BEARING PLATE
ROTARY SNUBBER
ANCHOR PLATE ASSEMBLY
HOLD-OPEN COLLAR
COMPRESSION SPRING
RELEASE HANDLE

FWD
LOWER SHAFT
LOWER
BEARING PLATE

GUIDE PLATE
LOWER HINGE ARM
GUIDE PLATE
GUIDE ARM BELLCRANK LINK
DOOR 1
A

Main Entry Door Body Torque Tube
Figure 3 (Sheet 2)

C72014
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 ALL  ú ú 02 Page 11 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

BELLCRANK LINK
UPPER  GUIDE ARM 
HINGE ARM 
GUIDE PLATE 

UPPER SLEEVE
RELEASE LEVER
HOLD-OPEN FITTING
ANCHOR
PLATE ROTARY SNUBBER
LOWER SLEEVE
LOWER LOWER LINKHINGE ARM
DOOR 5
B
Main Entry Door Body Torque Tube Figure 3 (Sheet 3)
C72018
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 ALL  ú ú 02 Page 12 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

UPPER LINING 
WINDOW REVEAL  ASSIST HANDLE 
CENTER LINING  DOOR INTERIOR HANDLE 
LOWER LINING 
SWEEPER SEAL  UPPER GATE 
INTERIOR  HINGE COVER 
HINGE LINK COVER 
BODY TORQUE TUBE ACCESS PANEL HINGE FLAP  HANDLE RELEASE BUTTON EXTERIOR HANDLE 
LOWER GATE 
FWD 
EXTERIOR 
Main Entry Interior and Exterior Views Figure 4 

C72022
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (2)  
Initial rotation of the interior handle rotates the control cam which transmits angular movement to the latching crank. The latching crank, connected to two pushrods, rotates the upper and lower latch torque tubes. Rotation of the latch torque tubes withdraws the latch rollers from the latch cams and folds the upper and lower gates inward. Withdrawal of the latch rollers closes the door warning switch and energizes the annunciator light on the flight engineer's panel.
　
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本文鏈接地址：747-400 AMM 飛機維護手冊 艙門 DOORS 1(24)