• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-14 10:14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

SEE ALATCH FITTING
GUIDE ROLLER AFT
1
GUIDE
ROLLER
RAMP

SHIM
LATCH
FITTING
FWD GUIDE ROLLER
A
Guide Roller Adjustment Figure 506
RAMP
CHANNEL

FORWARD GUIDE ROLLER RAMP
SHIM
LATCH
FITTING
4.31
INCHES
4.27
H36687
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-32-00
 ALL  ú ú 04 Page 518 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

ROTARY ACTUATOR
ARM AND LINK
(2 LOCATIONS)

SEE A
GEARBOX AND BRAKE ASSEMBLY (2 LOCATIONS)
LIFT
POWER UNIT
FWD
DOOR DOWN STOP
ROTARY
ACTUATOR

0.20 INCH
ADJUSTABLE END OF LINK
ROTARY ACTUATOR ARM
ROTARY ACTUATOR SLIP JOINT
LINK
DOOR END OF LINK
UP STOP
A
Lift Mechanism Adjustment
Figure 507

H36692
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-32-00
 ALL  ú ú 03 Page 519 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 
MAINTENANCE MANUAL 
AFT GEARBOX 
AND BRAKE ASSEMBLY 
FORWARD 
GEARBOX AND 
BRAKE ASSEMBLY 

SEE  A 
GEAR BOX 

BRAKE 
TORQUE WRENCH 
ADAPTER 
TORQUE 
WRENCH 
A  LOCK BOLT 
BRAKE HOUSING 
TORQUE 
ADJUSTING 
RING 
GEAR 
BOX 
A-A 
Brake Assembly Adjustment 
Figure 508 

H36695
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-32-00
 ALL  ú ú 03 Page 520 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

Not Used
Figure 509

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-32-00
 ALL  ú ú 04 Page 521 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H36700
A 747-400 MAINTENANCE MANUAL 
STOPS INTERNAL  HOOK  STOPS INTERNAL 


HOOK ACTUATOR DIAGRAM
NOTE: THE TURNS ARE THE NUMBER OF TURNS OF A TORQUE WRENCH IN THE MANUAL DRIVE. COUNT THE TURNS AFTER YOU FIND THE INTERNAL STOPS.

USE A TORQUE WRENCH TO FIND THE
INTERNAL STOPS OF THE ACTUATOR AS FOLLOWS:

1.  
MEASURE THE TORQUE (M) WHILE YOU MANUALLY TURN THE ACTUATOR. (THE TORQUE SHOULD BE CONSTANT WITHIN |2 POUND-INCHES).

2.  
TURN THE ACTUATOR UNTIL THE TORQUE INCREASES BY 15-20 POUND-INCHES (M + 15).

3.  
TURN THE ACTUATOR 1/2-TURN IN THE OPPOSITE DIRECTION FROM THE (M + 15) POINT.

4.
THE INTERNAL STOPS ARE AT THIS POINT.
INITIAL SWITCH ADJUSTMENT ONLY. SEE THE TEXT FOR THE FINAL ADJUSTMENT.

 

Latch and Hook Actuator Internal Stop and Rig Positions
Figure 510 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-32-00
 ALL  ú ú 04 Page 522 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H36739
A
747-400
MAINTENANCE MANUAL

EXTERNAL STOPS EXTERNAL CONTACTED AND STOPS RIGGED CLOSED CONTACTED
1
(M + 15)

1
MANUAL DRIVE CRANKING TORQUE
 
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 2(85)