(e) Remove the unwanted sealant with CLEANING AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003). Subtask 52-11-21-420-060 R K. Adjustment of the Tension of the Compensation Mechanism
 (Ref. Fig. 401/TASK 52-11-21-991-012)
 NOTE : It is necessary to adjust the tension of the torsion bar only if

____
 these components have been removed:
 - outer control handle

 -gearbox
 -upper and lower connection links
 -compensation mechanism
 -reducer shaft. R (1) Use a dynamometer to measure the load on the inner control handle.
 (2)
 Adjust the tension of the torsion bar to get a load less than or equal to 16 daN (35.9694 lbf) to open and close the door with the inner control handle.

 (3)
 To do this, turn the screw (1).

 (4)
 Safety the screw (1) with MISCELLANEOUS (Material No. 19-010).

 1EFF : ALL 1 52-11-21Page 487 1 1 Feb 01/03 1 1 1CES 1

 5. Close-up
________ Subtask 52-11-21-820-052
 A. Adjustment
 (1) Do an adjustment of the door locking mechanism (Ref. TASK 52-11-21-820-001).
 Subtask 52-11-21-640-050
 B. Lubrication
 (1)
 Lubricate the ends of the girt bar with COMMON GREASE (Material No. 04-004).

 (2)
 Lubricate the mating surfaces of the girt bar and the girt bar fittings with COMMON GREASE (Material No. 04-017).

 Subtask 52-11-21-916-050
 C. Protective Treatment
 (1)
 Apply STRUCTURE PAINTS (Material No. 16-001) to the ends of the screw threads and heads.

 (2)
 Apply another coat of STRUCTURE PAINTS (Material No. 16-002).

 (3)
 Apply SPECIAL MATERIALS (Material No. 05-002) to the screws of the mechanism.

 (4)
 Apply STORAGE PRESERVATION (Material No. 15-007) to the metal parts which are not painted.

 (5)
 Apply a coat of STORAGE PRESERVATION (Material No. 15-004) to all the parts installed.

 1EFF : ALL 1 52-11-21Page 488 1 1 Feb 01/02 1 1 1CES 1

 **ON A/C 001-002,

 Subtask 52-11-21-410-060
 D. Installation of Components
 (1)
 Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).

 (2)
 Install the door insulation.

 (3)
 Install the escape slide (Ref. TASK 25-62-44-400-001).

 (4)
 Install the door lining panels (Ref. TASK 25-23-46-400-001).

 (a)
 For the FWD passenger crew/door 831 831AZ, 831BZ, 831CZ, 831DZ, 831EZ.

 (b)
 For the passenger crew/door 841 841AZ, 841BZ, 841CZ, 841DZ, 841EZ.

 (5) Install the lining flap (Ref. TASK 52-11-31-400-001). R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-11-21-410-060-A
 D. Installation of Components
 (1)
 Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).

 (2)
 Install the door insulation.

 (3)
 Install the door lining panels (Ref. TASK 25-23-46-400-001).

 (4)
 Install the escape slide/raft (Ref. TASK 25-62-44-400-001).

 (a)
 For the FWD passenger crew/door 831 831AZ, 831BZ, 831CZ, 831DZ, 831EZ.

 (b)
 For the passenger crew/door 841 841AZ, 841BZ, 841CZ, 841DZ, 841EZ.

 (5)
 Install the lining flap (Ref. TASK 52-11-31-400-001).

 1EFF : ALL 1 52-11-21Page 489 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 Subtask 52-11-21-865-059
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
 Subtask 52-11-21-410-061
 F. Close Access
 (1)
 Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).

 (2)
 Remove all the ground support equipment, the maintenance equipment, the standard and special tools and all other items.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (4)
 Close the passenger/crew door (Ref. TASK 52-10-00-410-001) 831 or

 841.

 (5)
 Remove the access platform(s).

 1EFF : ALL 1 52-11-21Page 490 1 1 Feb 01/02 1 1 1CES 1 MECHANISM - DOOR LOCKING - ADJUSTMENT/TEST

__________________________________________
 TASK 52-11-21-820-001
 Adjustment/Test of the Door Locking Mechanism of the FWD Passenger/Crew Door
 1.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門2(9)