R
3. Job Set-up__________
R
Subtask 52-51-00-860-080
A. Aircraft Maintenance Configuration
(1) Make sure that access to the cockpit is available.
(2) Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
Subtask 52-51-00-865-069
R B. Open, safety and tag this(these) circuit breaker(s): 1MQ.
4. Procedure_________
R
Subtask 52-51-00-440-053
A. Reactivation of the Key Pad (Ref. Fig. 401/TASK 52-51-00-991-001)
(1) Cut and remove the tie-wrap to release the temporarily attached connector (4).
(2) Remove the blanking caps from the electrical connector (4) and receptacle (3).
(3) Connect the electrical connector (4) to the receptacle (3).
(4) Carefully install the control unit (1) and tighten the captive screws (2).
Subtask 52-51-00-865-070
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MQ.
Subtask 52-51-00-810-052
C. Fault Isolation Procedure
(1) Do the trouble shooting of the cockpit door lock system (Ref. TSM 52-51-00-810-801).
R (2) Do the operational test of the cockpit door locking system (Ref. TASK 52-51-00-710-002).
5. Close-up________
R
Subtask 52-51-00-862-051
A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R
TASK 52-51-00-040-010
Deactivation 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. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 24-41-00-861-002 24-41-00-862-002 52-51-00-710-001 52-51-12-000-001 ESPM 204825 AWM 52-51-02 52-51-00-991-011 Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerOperational Test of the Routine AccessRemoval of the Electric Release StrikeFig. 402
R
3. Job Set-up__________
R
Subtask 52-51-00-010-055
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.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
122VU DOORS/PAX/MONG 1MQ 13 T
R
4. Procedure
_________ R Subtask 52-51-00-040-058
A. Deactivation of the Electrical Release Strike
(Ref. Fig. 402/TASK 52-51-00-991-011)
(1)
Turn the D-ring of the latch mechanism and open the cockpit door.
(2)
Manually move the catch of the defective electrical release strike to check that it moves freely.
(3)
If the plunger causes a blockage of the catch, remove the defective electrical release strike (Ref. TASK 52-51-12-000-001).
NOTE : Do not disconnect the jiffi junction connectors at the A/C
____ wire harness for isolation reasons to prevent a short circuit.
(4) If the catch moves freely, disconnect the A/C wire harness from the applicable electrical release strike cables (Ref. ESPM 204825) and (Ref. AWM 52-51-02).
NOTE : Do not disconnect the jiffi junction connectors at the A/C
____ wire harness for isolation reasons to prevent a short circuit.
(5)
Make sure that the remaining electrical release strikes operate satisfactorily (Ref. TASK 52-51-00-710-001).
(6)
Put a warning notice on the door post to tell persons that the applicable elecrtical release strike is deactivated or removed.
1EFF : ALL 1 52-51-00Page 428 1 1 May 01/04 1 1 1CES 1
Electrical Release Strikes Figure 402/TASK 52-51-00-991-011
1EFF : 1 1R 1CES ALL 1 11 1 52-51-00 Page 429 May 01/04
Subtask 52-51-00-865-086
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MQ.
R
5. Close-up
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