• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-21 08:06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

 (h)  
Write down the airplane input voltage shown on the DVM.

 (i)  
Use the formula that follows to calculate the necessary transducer output:


 NOMINAL OUTPUT .............. x Measured input = Measured output of transducer NOMINAL INPUT (DVM voltage (PAV voltage reading)
 reading)
 0.0481 ...... x V at DVM = V at PAV
 26.00
 where V = voltage shown on monitor
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-00
 ALL  ú ú 08 Page 546 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 (j)  Loosen the clamping nut on the transducer clamp such that the
 transducer body can turn.
 (k)  Turn the body until there is an in-phase absolute output
 voltage of less than 1.25v ac.
 NOTE: The zero mark on the body must be less than 30 degrees____
 from the zero mark on the shaft.
 (l)  Tighten the clamping nut.
 (m)  Make sure that the absolute output in-phase voltage is less
 than 1.25v ac.
 (n)  Remove the lockwire from the control rod that is attached to
 the sensor crank.
 (o)  Turn the adjustment nut on the control rod slowly until the PAV
 shows a value near the value obtained by the formula.
 (p)  Use the breakout box and repeat the same adjustment steps for
 the other two neutral shift transducers.
 (q)  Turn the feel unit input crank clockwise approximately
 5-degrees.
 (r)  With the crank held at 5-degrees, measure the in-phase output
 of each transducer.
 (s)  Make sure that the voltage is in-phase with the input voltage.
 (t)  Make sure that the difference in the voltage between two
 transducers is not more than 0.40v ac.
 (u)  Turn the feel unit input crank counterclockwise approximately
 2-degrees.
 (v)  With the crank held at 2-degrees, measure the in-phase output
 of each transducer.
 (w)  Make sure that the voltage is in-phase with the input voltage.
 (x)  Make sure that the difference in the voltage between two
 transducers is not more than 0.40v ac.
 (y)  Put a lockwire on the control rod.
 (z)  Make sure that the PAV shows the necessary output voltage.

 (aa) Open these circuit breakers on the P11 panel and attach DO-NOT-CLOSE tags: 1) 11E17, FLT CONT COMPUTER POWER LEFT
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-00
 ALL  ú ú 07 Page 547 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 2) 11E20, FLIGHT CONT CMPTR PWR CENTER
 3) 11E35, FLT CONT CMPTR PWR RIGHT
 (ab) Disconnect the breakout box and the -26 cable assembly from the
 electrical connector.
 (ac) Disconnect the DVM and the PAV from the breakout box.
 (ad) Disconnect the breakout box and the -27 cable assembly from the
 transducer.
 S 825-054
 (5)  
Neutral Shift Transducer Adjustment (PROCEDURE 4):

 (a)  
Prepare the phase synchronous voltmeter for use as written on the tool.

 (b)  
Attach the applicable cable assembly from the voltmeter to the transducer connector.

 (c)  
Loosen the clamping nut on the transducer clamp such that the transducer body can turn.

 (d)  
Turn the body until there is an in-phase absolute output voltage of less than 1.25v ac.


 NOTE: The zero mark on the body must be less than 30 degrees
____
 from the zero mark on the shaft.

 (e)  
Tighten the clamping nut.

 (f)  
Make sure that the absolute output in-phase voltage is less than 1.25v ac.

 (g)  
Remove the lockwire from the control rod that is attached to the sensor crank.

 (h)  
Turn the adjustment nut on the control rod to get the smallest possible in-phase voltage.
 
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 飞行操纵 FLIGHT CONTROLS 3(22)