**ON A/C ALL
4. Procedure
_________ Subtask 52-51-00-710-056
A. Operational Test of the Emergency Access
(1) Do this test
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1. On Forward Attendant Panel (FAP) 120RH: In the Cockpit:
- enter the numerical emergency entry code and press the pushbutton '#' on the key pad 25MQ. - the buzzer 23MQ at the cockpitceiling panel operates.
On the COCKPIT DOOR panel 119VU: - the OPEN lamp of the indication light 22MQ flashes
On the Key Pad 25MQ: - the green LED flashes
On the Cockpit Door:
- wait for a defined period of time (adjustable between 15 sec. and 2 min.) to simulate no "flight crew reaction". - the solenoids of the electricalrelease strikes 30MQ, 31MQ and 32MQare de-energized.- the cockpit door is in the UNLOCK condition for 5 sec.
On the COCKPIT DOOR panel 119VU:
NOTE : There are two standards of the____ control unit 24MQ, P/N AR4709-1 and AR4709-3.
- with P/N AR4709-1, the OPEN and the FAULT lamps of the indication light 22MQ come on for 5 sec.
1EFF : ALL 1 52-51-00Page 517 1 1 Nov 01/04R 1 1 1CES 1
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ACTION RESULT -------------------------------------------------------------------------------
-with P/N AR4709-3, the OPEN lamp of the indication light 22MQ comes on for 5 sec.
On the Key Pad 25MQ:
-
the green LED come on for 5 sec.
In the cockpit:
-
the buzzer 23MQ at the cockpit ceiling 210RH stops.
2. On the Cockpit Door: On the Cockpit Door:
- open the cockpit door and close - the cockpit door moves in the open it again. direction and back in its locked position.
5. Close-up
________
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
Subtask 52-51-00-860-083
A. Put the aircraft back to the serviceable condition.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 52-51-00Page 518 1 1 May 01/05 1 1 1CES 1 **ON A/C ALL
TASK 52-51-00-720-001
Functional Test of the Door Opening Force
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific 1 SPRING BALANCE 10 DAN (24 LBF)
B. Referenced Information
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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 52-51-00-860-064
A. Aircraft Maintenance Configuration
(1)
Make sure that the cockpit door is closed.
(2)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
1EFF : ALL 1 52-51-00Page 519 1 1 May 01/04 1 1 1CES 1 Subtask 52-51-00-865-059
B. Make sure that this(these) circuit breaker(s) is(are) closed:
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PANEL DESIGNATION IDENT. LOCATION
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122VU DOORS/PAX/MONG 1MQ 13 T
R
4. Procedure
_________
R
Subtask 52-51-00-720-051
A. Functional Test of the Door Opening Force
(1)
Do this test to make sure that the top, center and bottom latch mechanism operate satisfactorily.
(2)
Measure the operation force necessary to open the cockpit door with a SPRING BALANCE 10 DAN (24 LBF).
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