(2)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
(3)
Make an entry in the aircraft technical log that the electrical release strike is deactivated.
1EFF : ALL 1 52-51-00Page 430 1 1 May 01/04 1 1 1CES 1R
TASK 52-51-00-440-010
Reactivation of the Electrical Release Strikes
1. Reason for the Job
__________________
Refer to the MMEL TASK: 52-50-02-J)
DOORS - Fixed Interior
Cockpit Door Locking System (CDLS)
Door Release Strike (Catch, Spring,
Solenoid, Bold)
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
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
52-51-00-710-001 Operational Test of the Routine Access
52-51-12-000-001 Removal of the Electric Release Strike
52-51-12-400-001 Installation of the Electric Release Strike
R 52-51-00-991-011 Fig. 402
1EFF : ALL 1 52-51-00Page 431 1 1 May 01/04 1 1 1CES 1 1EFF : ALL 1 52-51-00Page 432 1 1 May 01/04 1 1 1CES 1 Subtask 52-51-00-710-058
R
3. Job Set-up__________
R
Subtask 52-51-00-860-096
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
(2) Make sure that access to the flight compartment is available.
Subtask 52-51-00-865-087
R B. Open, safety and tag this(these) circuit breaker(s): 1MQ.
4. Procedure_________
R
Subtask 52-51-00-440-055
A. Reactivation of the Electrical Release Strike (Ref. Fig. 402/TASK 52-51-00-991-011)
(1) If removed, install the new electrical release strike (Ref. TASK 52-51-12-400-001).
(2) If not removed, replace the defective electrical release strike (Ref. TASK 52-51-12-000-001) and (Ref. TASK 52-51-12-400-001).
Subtask 52-51-00-865-082
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MQ.
C. Operational Test
(1) Do the operational test to make sure that the CDLS operates
satisfactorly (Ref. TASK 52-51-00-710-001). R
5. Close-up
________ R Subtask 52-51-00-860-103
A. Put the aircraft back to its initial configuration.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
(3)
Remove the deactivation entry from the aircraft technical log.
1EFF : ALL 1 52-51-00Page 433 1 1 May 01/04 1 1 1CES 1
R TASK 52-51-00-040-011 Check of the Pressure Rate Sensor
1. Reason for the Job
__________________
Refer to the MMEL TASK: 52-50-02-K)a)
DOORS - Fixed Interior
Cockpit Door Locking System (CDLS)
Pressure Rate Sensor
On Normal CKPT DOOR CONT Panel
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 PUMP - VACUUM
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
3. Job Set-up
__________ R Subtask 52-51-00-860-097
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(34)
