• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-06 23:10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 C ZERK
RUDDER HINGES NO. 2 AND 3
BMS 3-33
SEE B FWD
(2 LOCATIONS)
RUDDER HINGE NO. 6
RUDDER RUDDER HINGE NO. 1
RATIO  2 POINTS 
CHANGER  SEE  D 
SEE  E  A 

RUDDER HINGE ZERK
FWD BMS 3-33
(1 LOCATION PER HINGE, 6 HINGES)
RUDDER HINGE NO. 2, 3, 7, 8
1 POINT
B

Rudder and Rudder Trim Control System Lubrication
Figure 301 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-17
 ALL  ú ú 01 Page 302 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

FEEL AND CENTERING SPRINGS
BMS 3-33 (4 LOCATIONS)
RUDDER TRIM, FEEL AND CENTERING MECHANISM
4 POINTS
C

OUTPUT
RUDDER HINGE CONTROL ROD
(EXAMPLE)
ZERK

BMS 3-33 (1 LOCATION)
RUDDER HINGE ZERK
OUTPUT CONTROL ROD TO RUDDER BMS 3-33 POWER CONTROL
INPUT
MODULE
FWD  (1 LOCATION PER CRANK HINGE, 6 HINGES)
RUDDER HINGE NO. 1, 4, 5, 9, 10, 11 RUDDER RATIO CHANGER 1 POINT 1 POINT DE
Rudder and Rudder Trim Control System Lubrication Figure 301 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-17
 ALL  ú ú 01 Page 303 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

UPPER RUDDER ACTUATORS

Rudder and Rudder Trim Control System Lubrication
Figure 301 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-17
 ALL  ú ú 01 Page 304 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E29579
A
747-400
MAINTENANCE MANUAL

 (b)  
Manually move the upper and lower rudders fully right (or left) to get access to the lubrication points.

 (c)  
Release the rudder pedal.

 (d)  
Attach DO-NOT-OPERATE tags to the hydraulic system.


 S 843-026
 (2)  To prepare the rudder for lubrication with the hydraulic power, do these steps:
 (a)  
Do this task: "Supply Electrical Power" (Ref 24-22-00/201).

 (b)  
Do this task to pressurize the hydraulic system No. 1 and 4: "Supply Hydraulic Power" (Ref 29-11-00/201).

 (c)  
Open these access panels 324DL/324FL (lower rudder) and 324UL (upper rudder) (Ref 06-09-07/201).


 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE
_______ RUDDER CONTROL SURFACES AND THE NOSE LANDING GEAR BEFORE YOU PUSH THE RUDDER PEDAL. THE RUDDERS AND THE LANDING GEAR CAN MOVE QUICKLY WHEN YOU PUSH THE RUDDER PEDAL. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (d)  
Push and hold the captain's right (of left) rudder pedal fully forward.

 (e)  
Remove the hydraulic power from all four hydraulic systems (Ref 29-11-00/201).

 (f)  
Set the FLT CONTROL HYD POWER - TAIL switches No. 1, 2, 3, and 4 on the Pilot's Overhead Maintenance Panel, P461, to SHUTOFF.

 (g)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 1)  P180 DC Power Distribution Panel a) 180E7 ELEV/RUD VLV SYS 2 b) 180E22 ELEV/RUD VLV SYS 4 c) 180H8 ELEV/RUD VLV SYS 1 d) 180H23 ELEV/RUD VLV SYS 3

 (h)  
Make sure the hydraulic pressure is zero.

 (i)  
Release the rudder pedal.


 F.  Lubricate the Rudder Hinges
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-17
 ALL  ú ú 04 Page 305 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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 SERVICING 2(50)