• 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

Put the PCA rod end (12) into the elevator spar fitting and install with a bolt (14), washers (15, 17), bushing (16), and nut (18) with BMS 3-33 grease. BMS 3-33 (recommended), BMS 3-24 (optional).

 S 434-037

 (9)  
Make sure that the run-on torque for the nut (18) is 90-400 pound-inches (10.2-45.2 newton-meters), then tighten the nut to 1300-2000 pound-inches (147-226 newton-meters).

 S 094-038

 (10)
 Remove the plugs from the hydraulic lines (10) and the caps from the PCA ports (9).

 S 434-039

 (11)
 Connect the hydraulic lines (10) to the PCA (9).

 S 434-040

 (12)
 Align the pogo rod (5) to the PCA summing lever and install the bolt (6), washer (7), and nut (8).


 NOTE: It is necessary to adjust the elevator PCA pogo rod if the
____ adjustment for the pogo rod was changed while it was disconnected (AMM 27-31-00/501).
 S 434-041
 (13)
 Connect the electrical connector to the PCA (9).

 (14)
 Remove the elevator PCA lockout equipment (Fig. 402).

 (15)
 Remove the DO-NOT-OPERATE tags from the control columns.


 S 094-042
 S 094-044
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-05
 ALL  ú ú 01 Page 412 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 864-043
 (16)
 Release the control columns and put them back to the center position.

 S 864-092

 (17)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:

 (a)  
11B19, STAB TRIM ALT (IF INSTALLED)

 (b)  
11C12, STAB TRIM SHUTOFF RIGHT

 (c)  
11C13, STAB TRIM SHUTOFF LEFT

 (d)  
11H11 or 11C05, STAB TRIM CONT L

 (e)  
11H17, FLT CONT SHUTOFF TAIL LEFT

 (f)  
11H18, FLT CONT SHUTOFF TAIL CTR

 (g)  
11H20, STAB TRIM CONT R

 (h)  
11H28, FLT CONT SHUTOFF TAIL RIGHT

 (i)  
11J10, PCU MON SENSOR

 (j)  
11J11, PCU MON MOD


 S 864-090
 (18)
 Move the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the NORM position.

 S 864-091

 (19)
 Put the L, R, and C FLT CONTROL SHUTOFF switches on the right side panel, P61, to the ON position.

 S 644-048

 (20)
 Fully lubricate the link bearing with BMS 3-33 grease before you adjust the PCA. BMS 3-33 (recommended), BMS 3-24 (optional).

 S 724-068

 (21)
 If you only replace one elevator PCA, then do these steps:

 (a)  
Pressurize the hydraulic system to one of the the PCAs that was not replaced (AMM 29-11-00/201).


 NOTE: The center hydraulic system supplies pressure to the
____ inboard PCA. The left hydraulic system supplies pressure to the middle PCA. The right hydraulic system supplies pressure to the outboard PCA.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-05
 ALL  ú ú 01 Page 413 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

(b)

(c)

(d)

(e)

(f)

(g)

(h)

(i)

(j)

(k)


757
MAINTENANCE MANUAL

Keep a record of the exact position of the elevator trailing
 edge at the index plate.
Remove hydraulic power from the PCA that was not replaced
 (AMM 29-11-00/201).
Supply hydraulic power to the other PCA that was not replaced
 (AMM 29-11-00/201).
Keep a record of the exact position of the elevator trailing
 edge at the index plate.
Remove hydraulic power from the PCA (AMM 29-11-00/201).
Supply hydraulic power to the replaced elevator PCA
 (AMM 29-11-00/201).
Keep a record of the exact position of the elevator trailing
 edge at the index plate.
Make sure that this position is +/- 0.05 inch (+/- 1.3 mm) from
 
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(79)