• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-30 06:52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

.  If problem persists, replace the rudder power control unit. 
.  If problem persists, replace yaw damper coupler. 
PR sol short  msg. no. 22-21010   PR sol /YDC/wrg  LATCHED: Note 3  TYPE:  Possible Causes: . Pressure reducer bypass valve 
.  Yaw damper coupler 
Troubleshooting: 
.  Verify resistance from D295 socket 31 to ground is 60 ohms. 
.  Verify wiring between D295 socket 31 and D7377 socket 1 at the pressure reducer bypass valve solenoid. 
.  Verify connection to ground from D7377 socket 2 at the pressure reducer bypass valve solenoid. 
.  Inspect electrical connectors for bent or broken pins, contamination, or damage. 
.  If problem persists, replace the pressure reducer bypass valve. 
.  If problem persists, replace yaw damper coupler. 

500 
May 01/99   BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  22-12-01 Page 107 


YDC/solenoid/wiring/power/ faults 
YD sol low volt  msg. no. 22-21011  FDE: YD disenga  28V/sol/ YDC/wire  LATCHED: Note 3  TYPE: Note 2  Possible Causes: . Low 28 VDC voltage applied to yaw damper coupler . Yaw damper engage switch . Yaw damper coupler . Rudder power control unit actuator solenoid Troubleshooting: . Verify voltage to D295 socket 4 is between 22.0 and 29.5 volts DC with the yaw damper DC circuit breaker closed. . Verify resistance from D295 socket 14 to ground is less than 2.0 ohms with yaw damper engage switch in the OFF position. . Verify resistance from D295 socket 20 to ground is 60 ohms. . Verify wiring between D295 socket 20 and D291 socket 1 at the rudder power control unit actuator solenoid. . Verify connection to ground from D291 socket 2 at the rudder power control unit actuator solenoid. . Inspect electrical connectors for bent or broken pins, contamination, or damage. . If problem persists, replace yaw damper coupler. . If problem persists, replace the rudder power control unit actuator solenoid. 
PR sol low volt  msg. no. 22-21012   28V/sol/ YDC/wire  LATCHED: Note 3  TYPE: Note 2  Possible Causes: . Low 28 VDC voltage applied to the yaw damper coupler . Pressure reducer bypass valve . Yaw damper coupler Troubleshooting: . Verify voltage to D295 socket 4 is between 22.0 and 29.5 volts DC with the yaw damper DC circuit breaker closed. . Verify resistance from D295 socket 31 to ground is 60 ohms. . Verify wiring between D295 socket 31 and D7377 socket 1 at the pressure reducer bypass valve solenoid. . Verify connection to ground from D7377 socket 2 at the pressure reducer bypass valve solenoid. . Inspect electrical connectors for bent or broken pins, contamination, or damage. . If problem persists, replace yaw damper coupler. . If problem persists, replace the pressure reducer bypass valve. 

500 
22-12-01  May 01/99 
Page 108 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

EHSV faults 
YD EHSV fault msg. no. 22-21013  FDE: YD disenga  YD EHSV /wrg/YDC  LATCHED: Note 3  TYPE: Note 2  Possible Causes: . Rudder power control unit transfer valve . Yaw damper coupler 
Troubleshooting: 
. Verify resistance between D295 socket 30 and D295 socket 32 is 2K ohms. 
. Verify wiring between D295 and the rudder power control unit transfer valve: D295 socket 30 and D291 socket 8 
D295 socket 32 and D291 socket 5 
. Verify wiring between D291 socket 7 and D291 socket 6 at the rudder power control unit transfer valve. 
. Inspect electrical connectors for bent or broken pins, contamination, or damage. . If problem persists, remove and replace rudder power control unit transfer valve. . If problem persists, replace yaw damper coupler. 


26 VAC faults
YDC  msg. no.  FDE: LVDT/DAA/  LATCHED:  TYPE: Note 
26V AC  22-21014  YD disenga wrg/YDC  Note 3  2 
fault 

Possible Causes:
.  
Rudder power control unit position
transducer


.  
Yaw damper coupler


Troubleshooting:
.  
Verify resistance between D295 socket 9
and D295 socket 1 is 100 ohms.


.  
Verify wiring between D295 socket 9 and D295 socket 10 at the rudder power control unit position transducer.

.  
Verify connection to ground at D295 
socket 1.


.  
Verify connection to ground at D291 socket 9 at the rudder power control unit position transducer.

.  
Inspect electrical connectors for bent or
broken pins, contamination, or damage.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737 AMM 飞机维护手册 AUTO FLIGHT 自动飞行 2(57)