• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 00:06来源:蓝天飞行翻译 作者:admin
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

_______ CONNECT THE ELECTRICAL WIRES. INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
 (a) Connect the electrical connectors of the strike harness (3) to the electrical connectors (13) of the fuselage wire harness (2) (Ref. ESPM 204825) (Ref. AWM 52-51-02).
 (7)
 Put the cover plate (5) on the lavatory wall housing (1) and install the screws (4).

 (8)
 Put the cover profile (7) on the lavatory wall (8) and install the screws (6).


 1EFF : ALL 1 52-51-12Page 412 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 211-299, 301-399, 401-499,


 Subtask 52-51-12-820-050
 B. Adjustment
 (1)
 Make sure that the cockpit door is correctly adjusted (Ref. TASK 52-51-00-820-001).

 (2)
 Adjust the electrical release strikes in accordance with the cockpit door position (Ref. TASK 52-51-00-820-001).


 **ON A/C ALL
 Subtask 52-51-12-865-052
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MQ.
 Subtask 52-51-12-720-052
 D. Do the operational test of the cockpit door lock system (Ref. TASK 52-51-00-710-002).
 5. Close-up
________
 Subtask 52-51-12-860-052

 A. Put the aircraft back to the serviceable condition.
 (1)
 Make sure that the cockpit door is closed.

 (2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 1EFF : ALL 1 52-51-12Page 413 1 1 Aug 01/05 1 1 1CES 1


 BUZZER - COCKPIT DOOR LOCKING SYSTEM (23MQ) - REMOVAL/INSTALLATION
__________________________________________________________________ TASK 52-51-13-000-001 Removal of the Buzzer of the Cockpit-Door Locking System
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 25-13-41-000-001 Removal of the Ceiling Panels 52-51-13-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 52-51-13-860-051
 A. Aircraft Maintenance Configuration
 (1) Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 1EFF : ALL 1 52-51-13Page 401 1 1 May 01/05R 1 1 1CES 1


 Subtask 52-51-13-865-050
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU LIGHTING/EMER LT/CKPT/DOME 1LE H08 122VU LIGHTING/CKPT/DOME 3LE Y06
R **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
 122VU DOORS/PAX/MONG 1MQ T13 **ON A/C ALL
 4. Procedure
_________
 (Ref. Fig. 401/TASK 52-51-13-991-001)
 Subtask 52-51-13-010-051

 A. Removal of the Ceiling Panel
 (1) Remove the ceiling panel 211HC (5) (Ref. TASK 25-13-41-000-001). Subtask 52-51-13-020-050
 B. Removal of the Buzzer
 (1)
 Disconnect the cable terminals (1) and (2).

 (2)
 Remove the screws (4).

 (3)
 Remove the buzzer (3).


 1EFF : ALL 1 52-51-13Page 402 1 1 Aug 01/05 1 1 1CES 1


 Buzzer of the Cockpit-Door Locking System Figure 401/TASK 52-51-13-991-001 
R 1EFF : 1 1 1CES  ALL  1 111 52-51-13 Page 403 Feb 01/03

 

R
 TASK 52-51-13-400-001
 Installation of the Buzzer of the Cockpit-Door Locking System
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  24-42-00-861-001 24-42-00-862-001 25-13-41-400-001 52-51-00-710-002 52-51-13-991-001  Energize the Ground Service Network from the External PowerDe-energize the Ground Service Network Supplied from the External PowerInstallation of the Ceiling PanelsOperational Test of the Cockpit Door Lock System (CDLS) Fig. 401 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM DOORS 舱门7(59)