• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-10 10:22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

 C.
Procedure


 S 865-015
 (1)
Do this task: "Supply Electrical Power" (AMM 24-22-00/201).

 S 865-016

 (2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
On the P6, Main Power Distribution Panel, 1) 6L19, TE FLAP ELEC CONT OTBD 2) 6L20, TE FLAP ELEC CONT INBD

 (b)  
On the Overhead Power Distribution Panel, P7, 1) 7C10, FLT CONT ELEC 2L AC 2) 7C11, FLT CONT ELEC 2L DC 3) 7C12, FLT CONT ELEC 1L AC 4) 7C13, FLT CONT ELEC 1L DC 5) 7C14, FLT CONT ELEC 1R AC 6) 7C15, FLT CONT ELEC 1R DC


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-58-01
 ALL  ú ú 01 Page 501 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 7) 7C16, FLT CONT ELEC 2R AC 8) 7C17, FLT CONT ELEC 2R DC
 S 865-017
 (3)  Do this task: "Trailing Edge Flap Activation" (AMM 27-51-00/201). S 865-018
 WARNING:_______ MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
 FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP
 CONTROL LEVER.  WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL
 MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP
 CONTROL LEVER.  THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO

 EQUIPMENT.
 (4)  
Do this task to retract the TE flaps to the full up position: "Trailing Edge Flap Retraction with Hydraulic Power" (AMM 27-51-00/201).

 (a)  
Make sure the flap indicator bars of the FLAPS display on the EICAS change from green to magenta color when the flaps start to move.

 (b)  
Make sure the flap indicator bars change to green when the flaps are fully retracted.


 S 715-019
 (5)  
Make sure that the indication of the applicable TE FLAPS position on the EICAS flight controls maintenance page is -0.15 - 0.16 degree.

 S 865-020

 (6)  
Move the flap control lever to the 30-unit detent.

 (a)  
Make sure that the FLAPS display shows on the EICAS when you move the flap control lever. 1) The flap indicator bars will show in magenta color when the


 flaps start to move. 2) The flap indicator bars will change to green when the flaps are at the set position.
 S 715-021
 (7)  
Make sure that the TE flap position indication on the EICAS flight controls maintenance page is 28.69 - 31.32 degrees for the inboard flaps, and 28.31 - 31.70 for the outboard flaps.

 S 825-052

 (8)  
If it is necessary, adjust the flap position transmitter (AMM 27-58-01/401).

 S 865-022

 (9)  
Do this task to retract the TE flaps to the full up position: "Trailing Edge Flap Retraction with Hydraulic Power" (AMM 27-51-00/201).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-58-01
 ALL  ú ú 01 Page 502 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 415-023
 (10)
 Lift the access panel.

 S 865-024

 (11)
 If the electrical power is not necessary, do this task:  "Remove Electrical Power" (AMM 24-22-00/201).


 TASK 27-58-01-725-049
 3.  Operational Test of the RVDT Transmitter at the Flap Power Package__________________________________________________________________
 A. References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 27-51-00/201, Trailing Edge Flap System

 (3)  
IPC 27-51-09, Fig. 1

 (4)  
IPC 27-51-09, Fig. 3

 (5)  
SSM 27-58-01

 (6)  
AMM 27-58-01/401, Flap Position Transmitter

 (7)  
WDM 27-58-11

 B.
Access

 (1)  
Location Zone 137 Left Body Gear Wheel Well - Inbd Power Pack Transmitter 138 Right Body Gear Wheel Well - Outbd Power Pack Transmitter

 C.
Procedure


 S 865-041
 
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 飞行操纵 FLIGHT CONTROLS 6(22)