• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-14 10:11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

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

 

400
200
20
10
HANDLE POSITION (DEGREES) 0 246810 12
0 0
HANDLE POSITION 0

AT 16 INCH RADUIS 123
(INCHES)
PEAK UNLATCHING TORQUE
VS.
HANDLE POSITION

LEGEND:
SHORTEN UPPER GATE PUSHROD AND LENGTHEN

SPRING SCALE FORCE AT 18 INCHES RADIUS UPPER LATCH TORQUE TUBE PUSHROD.
TORQUE MEASURED WITH A TORQUE WRENCH LENGTHEN UPPER GATE PUSHROD AND UPPER
AND ADAPTER.
LATCH TORQUE TUBE PUSHROD.

HANDLE POSITION MEASURED MUST NOT INCLUDE SYSTEM FREEPLAY. REMOVE FREEPLAY PRIOR TO SHORTEN UPPER GATE PUSHROD. TAKING MEASUREMENT.
LENGTHEN UPPER GATE PUSHROD.
ADDITIONAL NORMAL ZONE FOR DOORS WITH
MAXIMUM PRESSURE SEAL DEFLECTION.

ZONE A - NO ADJUSTMENT NECESSARY.

RECOMMENDED TARGET TO AIM FOR IF ANY RIGGING
ADJUSTMENT IS MADE (300 POUND-INCHES, 5`)


Main Entry Door No. 1 Adjustment
Figure 501 (Sheet 6)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-01
 ALL  ú ú 04 Page 509 ú Feb 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F52383
A
747-400
MAINTENANCE MANUAL

GUIDE ARM LOWER HINGE CAVITY
(DOOR SHOWN IN THE OPEN POSITION
TO GIVE A BETTER VIEW)

Main Entry Door No. 1 Adjustment
Figure 501 (Sheet 7)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-01
 ALL  ú ú 04 Page 510 ú Jun 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F77930
A
747-400
MAINTENANCE MANUAL

TERMINAL

SPRING
WIRE BUNDLE RETRACTION MECHANISM


7.50 INCHES IS SATISFACTORY IF YOU DID NOT CHANGE THE RETRACTION MECHANISM AND THE RETRACTION MECHANISM OPERATES SMOOTHLY.
Main Entry Door 1 Adjustment Figure 501 (Sheet 8)
F52327
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-01
 ALL  ú ú 03 Page 511 ú Jun 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

DOUBLER (EXAMPLE)
0.00
-0.09

INCH -0.06


HINGE

WHEN YOU ADJUST THE UPPER GATE AGAINST NOTE: A POSITIVE FLUSHNESS SHOWS THE DOOR IS THE INSIDE OF THE BODY SKIN YOU ALIGN
OUTSIDE THE CONTOUR OF THE BODY SKIN.
THE FLUSHNESS IN THIS AREA.
A NEGATIVE FLUSHNESS SHOWS THE DOOR IS
INSIDE THE CONTOUR OF THE BODY SKIN.

THIS TOLERANCE IS FOR THE VERTICAL EDGE MEASURE FLUSHNESS ONLY IN AREAS WHERE
OF THE TOP AND BOTTOM HINGE COVERS. THIS DIMENSIONS ARE SHOWN.
TOLERANCE IS NOT FOR THE HORIZONTAL EDGES.
Door Flushness and Clearance Dimensions
Figure 502 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-01
 ALL  ú ú 03 Page 512 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D12301
A

747-400
MAINTENANCE MANUAL

HINGE ARM FLAP AND COVERS
(0.09 INCH MAXIMUM CLEARANCE) (2 LOCATIONS)

+0.18
INCH (BOTTOM GATE)+0.06
SKIN CLEARANCE DIMENSIONS
NOTE: YOU CAN ADD 0.02 INCH TO THE CLEARANCE FOR LESS THAN A TOTAL OF 20 INCHES.
THERE IS A SMOOTH CHANGE OF
CLEARANCES IN THIS AREA.

Door Flushness and Clearance Dimensions Figure 502 (Sheet 2)
D12310
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-11-01
 ALL  ú ú 03 Page 513 ú Feb 10/96
 
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 1(37)