52-13-21-820-001 Adjustment of the Locking Hook of the Aft
Passenger/Crew Door
**ON A/C 001-002,
52-10-00-991-011 Fig. 502 R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
52-10-00-991-011-A Fig. 502A
**ON A/C ALL
3. Job Set-up
__________
Subtask 52-10-00-010-055
A. Get Access WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE
_______
THAN 65 KNOTS.
WARNING : BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
_______
-
THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
-
THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES.
_______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
(1)
Put an access platform in position at zone 831 (841) or 832 (842).
(2)
Open the applicable passenger/crew door 831 (841) or 832 (842) (Ref. TASK 52-10-00-010-001).
(3)
Obey the special precautions before you start work on the door (Ref. TASK 52-10-00-860-001).
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B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
4. Procedure
_________ Subtask 52-10-00-410-056
A. Closing of the Door
(1) Close the passenger/crew door from the inner side. **ON A/C 001-002,
Subtask 52-10-00-720-055
B. Functional Check of the Locking Mechanism
(Ref. Fig. 502/TASK 52-10-00-991-011)
(1)
Operate the inner control handle and measure the load with a dynamometer 20 daN (44.9617 lbf).
(2)
Make sure that the load necessary to open and close the door is less than or equal to 16 daN (35.9694 lbf).
(3)
If it is necessary to adjust the door locking mechanism, do the test as follows:
(a)
Remove the escape slide on the FWD girt bar end (Ref. TASK 25-62-44-000-002).
(b)
Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
(c)
Operate the inner control handle and measure the load with a dynamometer 20 daN (44.9617 lbf).
(d)
Make sure that the load necessary to open and close the door is less than or equal to 16 daN (35.9694 lbf).
1EFF : ALL 1 52-10-00Page 512 1 1 May 01/05R 1 1 1CES 1
Inner Control Handle of the Passenger/Crew Door
Figure 502/TASK 52-10-00-991-011
R 1EFF : 001-002, 1 52-10-00Page 513 1 1 Feb 01/05 1 1 1CES 1
(e)
Adjust the door locking mechanism:
-
For the FWD passenger/crew door (Ref. TASK 52-11-21-820-001).
-
For the AFT passenger/crew door (Ref. TASK 52-13-21-820-001).
(f)
Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).
(g)
Install the escape slide on the FWD girt bar end (Ref. TASK 25-62-44-400-001).
R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-10-00-720-055-A
B. Functional Check of the Locking Mechanism
(Ref. Fig. 502A/TASK 52-10-00-991-011-A)
(1)
Operate the inner control handle and measure the load with a dynamometer 20 daN (44.9617 lbf).
(2)
Make sure that the load necessary to open and close the door is less than or equal to 16 daN (35.9694 lbf).
(3)
If it is necessary to adjust the door locking mechanism, do the test as follows:
(a)
Remove the escape slide/raft (Ref. TASK 25-62-44-000-002).
(b)
Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
(c)
Operate the inner control handle and measure the load with a dynamometer 20 daN (44.9617 lbf).
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