• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-14 10:24来源:蓝天飞行翻译 作者:航空
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

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú
 ú  01  Page 405
 ú  Feb 15/98 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (2)  AFT CARGO DOOR;
 Refer to the table that follows:

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 5 |Adapter | 52-34-06 | 02 | 530 | | | 6 |Clamp | | | 445 | | | 7 |Bellcrank | | | 510 | | | 8 |Clamp | | | 445 | | | 9 |Clamp | | | 390 | | | 13 |Torque Tube | | | 470 | | | 16 |Actuator (Latch Actuator) | | | 590 | | | 21 |Bolt (Mounting Bolt) | | | 535 | | | 22 |Washer | | | 550 | | | 23 |Nut | | | 555 | | | 24 |Nut | | | 465 | | | 25 |Washer | | | 460 | | | 26 |Nut | | | 410 | | | 27 |Washer | | | 405 | | | 28 |Washer | | | 400 | | | 29 |Bolt | | | 395 | | | 30 |Bolt | | | 450 | | | 31 |Washer | | | 455 | 2......…........…...................................…..........…......…........1
 D. References
 (1)  
12-21-04/301, Doors

 (2)  
20-22-01/601, Electrical Bonding

 (3)  
52-34-00/501, Forward/Aft Cargo Door

 (4)  
CMM 52-34-11 (Forward Cargo Door)

 (5)  
CMM 52-35-11 (Aft Cargo Door)

 (6)  
SSM 52-34-01, 52-35-01

 (7)  
WDM 52-34-11, 52-35-11

 E.
Access

 (1)  
Location Zone 122 Forward Cargo Container Compartment, Forward Half 142 Aft Cargo Container Compartment

 (2)  
Access Panel
 821R Door - Forward Cargo Compartment
 822R Door - Aft Cargo Compartment

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú
 ú  01  Page 406
 ú  Feb 15/98 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 F. Procedure
 S 014-022
 (1)  Disconnect the pushrods (12), (18), and (19) from the bellcranks (Fig. 401).
 NOTE: The pushrod (14) was disconnected during the removal of the
____
 latch actuator.

 S 724-023
 (2)  
Examine the torque necessary to turn each lower latch through its full range of motion.

 S 644-025

 (3)  
If the torque is more than 55 pound-inches, clean and lubricate the lower latches (Ref 12-21-04/301).

 S 354-026

 (4)  
If the torque is more than 55 pound-inches after you lubricate the lower latches, rework the latches per CMM 52-34-11 (Forward Cargo Door) or CMM 52-35-11 (Aft Cargo Door).

 S 414-024

 (5)  
Connect the pushrods (12), (18), and (19) to the bellcranks.


 NOTE: Pushrod (14) will be connected after the latch actuator is
____
 installed.

 S 824-033
 CAUTION: USE A TORQUE WRENCH WITH A DIAL INDICATOR TO FIND WHEN THE
_______ ACTUATOR INTERNAL STOPS ARE AGAINTS EACH OTHER. DO NOT USE MORE THAN 25 POUND-INCHES OF TORQUE. IF YOU USE MORE THAN 25 POUND-INCHES, YOU CAN CAUSE INTERNAL DAMAGE TO THE LATCH ACTUATOR.
 (6)  
Do these steps to set the latch actuator in the rigged open position:

 (a)  
Manually turn the latch actuator counterclockwise to the open position.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú ú 01 Page 407 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  Measure the torque.  When the torque increases by 15-20
 pound-inches, the internal steps are against each other.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 舱门 DOORS 3(72)