• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 15:00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

 (3)  
Open the applicable circuit breakers and attach DO-NOT-CLOSE tags:


 (a)  P6-2 Circuit Breaker Panel
 1) ELEC HYD PUMP CONT SYS A
 2) ELEC HYD PUMP CONT SYS B
 3) PRESS IND SYS A
 4) PRESS IND SYS B

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-15-71
 ALL  ú ú 01 Page 201 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 032-093
 (4)  
Disconnect the electrical connectors from the low pressure switch.

 S 032-094

 (5)  
Disconnect the hydraulic lines.

 S 682-095

 (6)  
Drain hydraulic fluid into a container.

 S 162-096

 (7)  
Clean all hydraulic fluid from the installation area if it is necessary (AMM 12-40-00/201).

 S 032-097

 (8)  
Install plugs to the hydraulic lines.

 S 032-098

 (9)  
Remove the unions and the protective plugs from the pressure module.


 (a)  Discard the O-rings.
 S 432-100
 (10)
 Install plugs in the open ports of the pressure module.

 S 032-101

 (11)
 Remove the mounting bolts.

 S 022-102

 (12)
 Remove the pressure module.


 TASK 29-15-71-402-103
 3. Hydraulic Systems A and B Pressure Module Installation
______________________________________________________
 A. Consumable Materials
 (1)  
D00567 Skydrol Assembly Lube - MCS 352

 (2)  
D00568 Fluid - Hydraulic, BMS 3-11


 B. References
 (1)  
AMM 12-12-00/301, Hydraulic Reservoir

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 29-15-00/201, Hydraulic Systems A, B and Standby


 C. Access
 (1)  Location Zone
 101 Control Cabin, LH
 102 Control Cabin, RH
 216 Main Wheel Well, LH
 217 Main Wheel Well, RH

 D. Procedure
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-15-71
 ALL  ú ú 01 Page 202 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 212-104
 CAUTION: MAKE SURE UNWANTED MATERIAL DOES NOT GO INTO THE MODULE PORTS
_______ OR THE HYDRAULIC LINES DURING THE INSTALLATION. THIS CAN CAUSE DAMAGE TO EQUIPMENT.
 (1)  
Make sure unwanted material does not go into the module ports or the hydraulic lines.

 S 642-105

 (2)  
Apply assembly lube or hydraulic fluid to the O-rings and the unions.

 S 432-106

 (3)  
Install the O-rings and the unions in the module ports.

 S 212-107

 (4)  
Make sure the plugs are in the correct ports.

 S 212-108

 (5)  
Make sure lockwires are installed.

 S 212-109

 (6)  
Make sure the check valve is installed in port 8 for the system A pressure module.

 S 422-110

 (7)  
Put the pressure module in its mounting position.

 S 422-120

 (8)  
Install the mounting bolts.

 S 032-111

 (9)  
Remove the plugs.

 S 432-112

 (10)
 Connect the hydraulic lines to the pressure module.

 (11)
 Connect the electrical connectors to the low pressure switches.

 (12)
 Supply electrical power (AMM 24-22-00/201).

 S 862-115

 (13)
 Remove the DO-NOT-CLOSE tags and close the applicable circuit breakers:


 S 432-113
 S 862-114
 (a)  P6-2 Circuit Breaker Panel
 1) ELEC HYD PUMP CONT SYS A
 2) ELEC HYD PUMP CONT SYS B

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 液压 HYDRAULIC POWER(115)