4. Procedure_________
Subtask 52-51-00-210-050
A. Check of the Flight-Deck-Door Lock-Solenoid
(1) Make sure that the cockpit door is closed and manually locked.
R R (2) Do this test to make sure that the electrical release strike operates correctly.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the cockpit door: In the door frame:
- push the cockpit door in the - the electrical release strike holds
flight direction the cockpit door in the closed
position.
2. In the cockpit, on the panel On the cockpit door:
111VU: - the electrical release strike
- push the switch COCKPIT DOOR. operates in the unlocked condition.
- push the cockpit door in the - the cockpit door moves in the open
flight direction direction.
3. On the panel 111VU: In the door frame:
- release the switch COCKPIT - the electrical release strike returns
DOOR. to its locked condition.
5. Close-up________
Subtask 52-51-00-860-051
A. Aircraft Maintenance Configuration
(1)
Put the aircraft back to the serviceable condition.
(2)
If the test is incorrect , make an entry in the aircraft technical log that the electrical release strike does not operate.
1EFF : 201-210, 1 52-51-00Page 402 1 1 Feb 01/03 1 1 1CES 1 1EFF : 201-210, 1 52-51-00Page 403 1 1 Aug 01/03 1 1 1CES 1 **ON A/C ALL
TASK 52-51-00-440-001
Reactivation of the Flight-Deck-Door Lock-Solenoid
1. Reason for the Job__________________
R R R R Refer to the MMEL TASK: 52-50-01 Doors Flight Deck Door Lock Solenoid (FAA Only)
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-51-12-400-001 Installation of the Electric Release Strike
3. Job Set-up__________
Subtask 52-51-00-860-052
A. Make sure that the access to the cockpit is available.
4. Procedure_________
Subtask 52-51-00-420-050
A. Replace the defective electrical release strike (Ref. TASK 52-51-12-400-001).
TASK 52-51-00-040-002
Deactivation of the Key Pad
1. Reason for the Job
__________________
Refer to the MMEL TASK: 52-50-02-1)b)
DOORS - Fixed Interior
Cockpit Door Locking System (CDLS)
Cockpit Door Toggle Switch Lock Function
(FAA Only)
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 R 52-51-00-991-001 Fig. 401
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R
3. Job Set-up__________
R
Subtask 52-51-00-860-053
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 cockpit is available.
Subtask 52-51-00-865-053
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU DOORS/PAX/MONG 1MQ 13 T
R
4. Procedure_________
R
Subtask 52-51-00-040-050
A. Deactivation of the Key Pad (Ref. Fig. 401/TASK 52-51-00-991-001)
NOTE : If the cockpit door closes during the deactivation procedure and____ no person is in the cockpit, de-energize the aircraft electrical circuits. This will let you open the cockpit door from the cabin.
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本文链接地址：A320飞机维护手册 AMM DOORS 舱门7(28)
