• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-11 09:19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

 1) 7F3 HYDRAULICS HYDIM 1
 2) 7G3 HYDRAULICS HYDIM 2
 3) 7H3 HYDRAULICS HYDIM 3
 4) 7J3 HYDRAULICS HYDIM 4

 

 S 034-006
 (5)  
Disconnect the electrical connector (2) from the temperature transmitter (1).

 S 024-007

 (6)  
Remove the transmitter (1) from the case drain module.

 S 034-008

 (7)
Remove the O-ring (3) from the temperature transmitter (1).

 S 034-023

 (8)  
Discard the O-ring (3).


 TASK 29-32-02-404-009
 3. Temperature Transmitter Installation (Fig. 401)
____________________________________
 A. Consumable Materials
 (1)  
D00567 Skydrol Assembly Lube - MCS 352

 (2)  
D00153 Fluid - Hydraulic, Fire-Resistant, BMS 3-11

 B.
Parts


 ~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Temperature Transmitter | 29-11-18 | 01 | 117 | | | 3 | Packing | | | 120J | 2......…........…...................................…..........….....….........1
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-32-02
 ALL  ú ú 03 Page 403 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 C. References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (3)  
AMM 54-62-00/201, Nacelle Strut Access Panels

 (4)  
AMM 54-62-02/501, Nacelle Strut Access Doors

 D.
Access

 (1)  
Location Zone
 454 System 1 - Strut Trailing Edge Fairing
 464 System 2 - Strut Trailing Edge Fairing
 474 System 3 - Strut Trailing Edge Fairing
 484 System 4 - Strut Trailing Edge Fairing


 (2)  
Access Panel
 454A Trailing Edge Fairing Doors - System 1
 464A Trailing Edge Fairing Doors - System 2
 474A Trailing Edge Fairing Doors - System 3
 484A Trailing Edge Fairing Doors - System 4


 E.
Procedure


 S 644-010
 (1)  
Apply some Skydrol assembly lube or hydraulic fluid to the O-ring (3).

 S 434-011

 (2)  
Install the O-ring (3) on the temperature transmitter (1).

 S 424-024

 (3)  
Install the temperature transmitter (1) in the case drain module.

 S 434-026

 (4)  
Tighten the temperature transmitter (1) to 250-300 pound-inches (28-33 N.m).

 (5)  
Safety the temperature transmitter (1) with a lockwire.


 S 434-025
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-32-02
 ALL  ú ú 03 Page 404 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-013
 (6)  Connect the electrical connector (2) to the temperature
 transmitter (1).
 S 864-014
 (7)  Close the circuit breaker for the applicable hydraulic system:
 (a)  P7 Overhead Circuit Breaker Panel
 1)  7F3 HYDRAULICS HYDIM 1
 2)  7G3 HYDRAULICS HYDIM 2
 3)  7H3 HYDRAULICS HYDIM 3
 4)  7J3 HYDRAULICS HYDIM 4

 S 864-015
 (8)
Pressurize the applicable hydraulic system (AMM 29-11-00/201).

 S 864-027

 (9)
Push the HYD switch on the display select panel for the EICAS.

 S 714-016

 (10)
 Make sure the HYD TEMP indication, for the applicable hydraulic system, shows the approximate temperature of the hydraulic system.

 S 794-017

 (11)
 Examine the temperature transmitter installation for leakage.

 S 364-018
 
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 液压 HYDRAULIC 2(118)