• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-06 23:21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

 2.  Remove The EAS Electrohydraulic Servovalve and the Solenoid Valve (Fig. 201)_________________________________________________________________
 A.  References
 (1)
06-09-05/201, Body Section 48 Access Doors and Panels

 (2)
20-11-19/401, O-Ring

 (3)
20-11-28/401, Lockwire

 (4)
24-22-00/201, Manual Control

 (5)
29-11-00/201, Main Hydraulic Supply System


 B.  Access
 (1)  
Location Zones 315 Area Aft of Stabilizer Box Compartment, LH 316 Area Aft of Stabilizer Box Compartment, RH

 (2)  
Access Panel
 315A Access Door

 

 C.  Remove the EAS Electrohydraulic Servovalve and Solenoid Valve
 S 862-052
 (1) Supply the electrical power (Ref 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-12-02
 ALL  ú ú 01 Page 201 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
EAS (3 PLACES)
SEE A
ACCESS
PANEL
315A
1.  SERVO ASSEMBLY
7.  O-RINGS
ELECTRICAL CONNECTOR
4.  GASKET PLATE
2.  SOLENOID VALVE 2 (ENGAGE)
2.  SOLENOID VALVE 1 (ARM)
6. WASHER
5.  SCREWS
3. ELECTROHYDRAULIC (4 EACH
(4 EACH
SERVOVALVE
VALVE)
VALVE)
A
EAS Electrohydraulic Servovalve and Solenoid Valves Installation Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-12-02
 ALL  ú ú 02 Page 202 ú Oct 10/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 862-053
 WARNING:_______ MAKE SURE THAT YOU MOVE PERSONS AND BLOCKAGES AWAY FROM THE
 CONTROL SURFACES.  THE CONTROL SURFACES CAN MOVE SUDDENLY WHEN
 YOU REMOVE THE HYDRAULIC POWER.  THIS CAN CAUSE INJURY TO

 PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  Remove the hydraulic pressure from the applicable hydraulic system (Ref 29-11-00/201).
 NOTE: The hydraulic system No. 1 supplies the power to the center
____ EAS. The hydraulic system No. 2 supplies the power to the right EAS. The hydraulic system No. 3 supplies the power to the left EAS.
 S 862-054
 (3)  
Set the No. 1, 2, 3, and 4 switches of the FLT CONTROL SHUTOFF TAIL VALVE to the SHUTOFF position. The switches are on the Pilots' Overhead Maintenance Panel, P461.

 S 862-083

 (4)  
Set the No. 1 and 2 switches of the STAB TRIM hydraulic to the CUTOFF position and attach the DO-NOT-OPERATE tags. The switches are on the Pilots' Control Stand.

 S 862-085

 (5)  
Open these circuit breakers and attach the DO-NOT-CLOSE tags:


 (a)  P7 Overhead Circuit Breaker Panel 1) 7D7, FLT CONT CMPTR L SERVO 2) 7D8, FLT CONT CMPTR L PWR 3) 7D12, FLT CONT CMPTR C SERVO 4) 7D13, FLT CONT CMPTR C PWR 5) 7D14, FLT CONT CMPTR R SERVO 6) 7D15, FLT CONT CMPTR R PWR
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-12-02
 ALL  ú ú 01 Page 203 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 7) 7E7, STAB TRIM L S/O VALVE
 8) 7E20, STAB TRIM R S/O VALVE

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

 S 012-057
 (6)  Open the 315A access door in the tail cone to get access to the EASs (Ref 06-09-05/201).
 S 162-087
 CAUTION: DO NOT LET THE CONTAMINATION GET INTO THE EAS AND THE VALVES.
_______ THE EAS AND THE VALVES ARE SENSITIVE ELECTROHYDRAULIC DEVICES. THE CONTAMINATION CAN CAUSE DAMAGE AND FAILURE TO THE EAS AND THE VALVES.
 
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 空调 AUTO FLIGHT(99)