• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-19 08:00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

 12-21-05
 ALL  ú ú 01 Page 304 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 (d)  11G27, CSEU 2R AC or FLT CONT ELEC 2R AC
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-05
 ALL  ú ú 01 Page 305 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL


STABILIZER-TRIM CONTROL SYSTEM


Stabilizer Control System Lubrication
Figure 301 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-05
 ALL  ú
 ú  01  Page 306
 ú  Jan 28/02 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

757
MAINTENANCE MANUAL

BALLNUT 
FOR THE TRIM 
BALLSCREW ACTUATOR 
ATTACHMENT GIMBALS 
ZERK  FOR THE TRIM 
ACTUATOR BALLSCREW 
OR BMS 3-33  1  ZERK 
MIL-G-23827  1 
BMS 3-33 
(2 LOCATIONS)  OR 
2  MIL-G-23827 
(4 LOCATIONS) 
ATTACHMENT GIMBALS 
FOR THE TRIM 
ACTUATOR BALLSCREW 
ZERK 

BMS 3-33 
OR  AFT 
MIL-G-23827 
8 POINTS  STABILIZER-TRIM 
(2 LOCATIONS)  UPPER GIMBAL 

STABILIZER-TRIM BALLSCREW ACTUATOR
ATTACHMENT GIMBALS FOR THE TRIM ACTUATOR BALLSCREW
ZERK
BMS 3-33
1
OR ATTACHMENT GIMBALS
MIL-G-23827 FOR THE TRIM
(2 LOCATIONS)ACTUATOR BALLSCREW
ZERK  AFT 

BMS 3-33 
OR MIL-G-23827  STABILIZER-TRIM LOWER GIMBAL  1  ONE MORE LUBE POINT IS ON THE OPPOSITE SIDE (NOT SHOWN) 
(4 LOCATIONS)  6 POINTS  2  PUT THE STABILIZER AT 15 UNITS OF 
TRIM FOR THE BEST ACCESS TO THE AFT 
C  LUBE FITTING ON THE UPPER GIMBAL 

Stabilizer Control System Lubrication
Figure 301 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-05
 ALL  ú ú 01 Page 307 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL


STABILIZER PIVOT BEARING SEE

Stabilizer Pivot Bearings Lubrication
Figure 302

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-05
 ALL  ú
 ú  01  Page 308
 ú  Jan 28/02 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

757 MAINTENANCE MANUAL
 RUDDER AND RUDDER TRIM CONTROL SYSTEM - SERVICING
_________________________________________________
 1. General
_______
 A. This procedure contains these tasks:
 -
Rudder Hinge and Yaw Damper Summing Lever - Lubrication

 -
Rudder PCA - Lubrication


 TASK 12-21-06-643-002
 2. Rudder Hinge and Yaw Damper Summing Lever - Lubrication
_______________________________________________________
 A. Equipment
 (1)  Rudder PCA Lockout Equipment - B27013-19
 B. Consumable Materials ú (1) D00633 Grease, Corrosion Preventive - BMS 3-33 (preferred) ú D00015 Grease, Corrosion Preventive - BMS 3-24 (optional)
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757 AMM 飞机维护手册 SERVICING 1(95)