737-300 400 500 AMM 飞机维护手册 舱门 DOORS 1(35)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

_______ WHEN THE DOOR IS CLOSED. IF THE FILLER PLUG IS NOT OUTBOARD WHEN THE DOOR IS CLOSED, DAMAGE TO THE AIRPLANE CAN OCCUR.
 c) Make sure the filler plug on the snubber is outboard when the door is closed. d) Use the bolt (18) to attach the fitting to the snubber. 2) Attach the radius link to the snubber if it is necessary. a) Use the bolt (22) to attach the radius link to the snubber. b) Install the washers, the nut and the cotter pin on the
 bolt. 3) Engage the radius link with the stop plates. 4) Connect the fitting (25) to the support (26) with four
 bolts.
 (b)  Connect the bottom hinge arm. 1) Put the thrust washer (23) between the hinge arm and the bottom stop plate.
 2)  Align the holes in the hinge arm, the radius link and the stop plates (20).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-00
 ALL  ú ú B01 Page 409 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 3) 4) 5) 6)  Assemble the bottom spigot. a) Put the spring, the washer and the O-ring on the bottom spigot.Align the marks on the bottom spigot with the marks on the hinge arm.Put the bottom spigot in the stop plate.Install the bolt that holds the hinge arm to the bottom spigot.
 (4)  S 434-020-B00Install the assist spring and the torque tube (AMM 52-11-41/401).
 (5)  S 434-022-B00Install the hinge arm covers, the stop pins, and the door seal.
 NOTE:____ It is only necessary to install these parts on a new door.
 (a) (b) (c)  Install the hinge arm covers 1) Put primer on the bolts that hold the hinge covers to the hinge arms. 2) Attach the hinge covers to the hinge arms with the bolts.Install the stop pins on the edges of the door. 1) Put a layer of corrosion preventive compound on the threads of the stop pins. 2) Put the stop pins on the door.Install the door seal (AMM 52-09-13/401).
 (6)  S 824-023-B00Do this task:  "Forward Entry Door Adjustment" (AMM 52-11-00/501).
 (7)  S 724-024-B00Do this task:  "Forward Entry Door Test" (AMM 52-11-00/501).
 (8)  S 434-025-B00Install the lining and the insulation on the forward entry door (AMM 52-11-31/401).
 (9)  S 434-026-B00Install the escape slide on the forward entry door (AMM 25-61-35/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-00
 ALL  ú ú B01 Page 410 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FORWARD ENTRY DOOR - ADJUSTMENT/TEST
____________________________________
 1.  General_______
 A. This procedure contains four tasks:
 (1)  
The operational test of the forward entry door

 (2)  
The adjustment of the forward entry door

 (3)  
A special adjustment to correct "soft unlatching"

 (4)  
The functional test of the forward entry door.

 TASK 52-11-00-705-003-B00
 2.  Forward Entry Door Operational Test___________________________________
 A. General
 (1)  
This test is an operational check of the forward entry door. It makes sure the door operates satisfactorily. This test does not make sure the door is adjusted correctly.

 B.
References

 (1)  
24-22-00/201, Manual Control

 C.
Access

 (1)  
Location Zone
 105 Forward Entry Door

 (2)  
Access Panel
 4201L Forward Entry Door

 D.
Procedure

 S 865-001-B00
 (1)  
Supply electrical power (Ref 24-22-00/201).

 S 715-002-B00

 (2)  
Use the external handle to open the forward entry door.

 (a)  
Pull the handle from the recess.

 (b)  
Turn the handle clockwise. 1) See that the door moves inboard. 2) See that the FWD ENTRY light on the P5 panel comes on.

 (c)  
Fully turn the handle clockwise (180 degrees). 1) See that the door moves to the cocked position.

 (d)  
　
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 舱门 DOORS 1(35)