• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-01 08:37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. General
_______
 A. This procedure provides these tasks:
 (1)  
Removal of the P5-17 temperature control module

 (2)  
Installation of the P5-17 temperature control module


 TASK 21-61-01-004-004
 2. Temperature Control Module Removal (Fig. 401)
__________________________________
 A. Access
 (1)  Location Zone
 102 Control Cabin - Right

 B. Procedure
 S 864-006
 (1)  
Make sure that the L and R PACK switches on the P5-10 air conditioning panel are set to OFF.

 S 864-007

 (2)  
Open all the circuit breakers on the P6-4 panel for the air conditioning system and the temperature control system and install DO-NOT-CLOSE tags.

 S 864-008

 (3)  
Open these circuit breakers on the P6-3 panel and install DO-NOT-CLOSE tags:

 (a)  
MASTER CAUTION (all except FUEL, if installed)

 (b)  
INDICATOR LIGHTS, MASTER DIM BUS (9 locations)

 (c)  
DIM & TEST (1 location)

 (d)  
NOSE GEAR AIR/GND

 (e)  
LANDING GEAR AIR/GND RELAY & LTS

 


 S 014-009
 (4)  
Lower the P5 panel to get access to the P5-17 temperature control module on the forward overhead panel in the flight deck.

 S 034-010

 (5)  
Disconnect all electrical connectors at the back of the P5-17 temperature control module.

 S 034-011

 (6)  
Loosen the 1/4 turn fasteners at the four corners of the P5-17 temperature control module that attach the module to the P5 forward overhead panel.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-61-01
 ALL  ú ú 02 Page 401 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
P5-17 CABIN TEMPERATURE MODULE
1/4 TURN FASTENER (4 LOCATIONS)

CABIN TEMPERATURE MODULE


Cabin Temperature Module Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-61-01
 ALL  ú
 ú  02  Page 402
 ú  Nov 15/96 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G16395
A 737-300/400/500MAINTENANCE MANUAL
 S 024-012
 (7)  Remove the P5-17 temperature control module.
 TASK 21-61-01-404-005
 3. Temperature Control Module Installation (Fig. 401)
_______________________________________
 A. References
 (1) AMM 36-05-00/201, Pressurize/Depressurize Pneumatic System
 B. Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right

 C. Procedure
 S 424-013
 (1)  
Put the P5-17 temperature control module in its position in the P5 forward overhead panel.

 S 434-014

 (2)  
Tighten the 1/4 turn fasteners that secure the temperature control module to the P5 forward overhead panel.

 S 434-015

 (3)
Install the electrical connectors at the back of the panel.

 S 414-016

 (4)  
Raise the P5 forward overhead panel to its installed position and secure the fasteners at the lower corners of the panel.

 S 864-017

 (5)  
Remove the DO-NOT-CLOSE tags on the P6-4 circuit breaker panel and close the circuit breakers for the air conditioning system and the tempeature control system.

 S 864-018

 (6)  
Remove the DO-NOT-CLOSE tags on the P6-3 circuit breaker panel and close these circuit breakers:

 (a)  
MASTER CAUTION (all except FUEL, if installed)

 (b)  
INDICATOR LIGHTS, MASTER DIM BUS (9 locations)

 (c)  
DIM & TEST (1 location)

 (d)  
NOSE GEAR AIR/GND

 (e)  
LANDING GEAR AIR/GND RELAY & LTS

 


 D. Temperature Control Module (P5-17) Test
 S 864-001
 
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 空调 AIR CONDITIONING 2(141)