Subtask 52-13-21-420-060
 K. Adjust the Tension of the Compensation Mechanism
 (Ref. Fig. 419/TASK 52-13-21-991-011)

 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.
 (1)
 Take a dynamometer capacity.

 (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 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 52-13-21Page 486 1 1 Feb 01/01 1 1 1CES 1

 Compensation Mechanism
 Figure 419/TASK 52-13-21-991-011
 1EFF :  ALL  1  52-13-21 Page 487 
1  1  Feb 01/01
 1  1
 1CES  1

 5. Close-up
________ Subtask 52-13-21-820-052
 A. Adjustment
 (1) Do an adjustment of the door locking mechanism (Ref. TASK 52-13-21-820-001).
 Subtask 52-13-21-640-050
 B. Lubrication
 (1)
 Lubricate the ends of the girt bar with No. 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 52-13-21-916-050
 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 52-13-21Page 488 1 1 Feb 01/02R 1 1 1CES 1

 **ON A/C 001-002,

 Subtask 52-13-21-410-060
 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 25-23-46-400-002).

 (a)
 For the passenger crew/door 832 832AZ, 832BZ, 832CZ, 832DZ, 832EZ.

 (b)
 For the passenger crew/door 842 842AZ, 842BZ, 842CZ, 842DZ, 842EZ.

 (5) Install the flap lining (Ref. TASK 52-13-31-400-001). R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-13-21-410-060-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 escape slide/raft (Ref. TASK 25-62-44-400-001).

 (4)
 Install the door panels lining (Ref. TASK 25-23-46-400-002).

 (a)
 For the passenger crew/door 832 832AZ, 832BZ, 832CZ, 832DZ, 832EZ.

 (b)
 For the passenger crew/door 842 842AZ, 842BZ, 842CZ, 842DZ, 842EZ.

 (5)
 Install the flap lining (Ref. TASK 52-13-31-400-001).

 1EFF : ALL 1 52-13-21Page 489 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 Subtask 52-13-21-865-059
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
 Subtask 52-13-21-410-061
 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) 832 or

 842.

 (5)
 Remove the access platform(s).

 1EFF : ALL 1 52-13-21Page 490 1 1 Feb 01/02R 1 1 1CES 1

 MECHANISM - DOOR LOCKING - ADJUSTMENT/TEST
__________________________________________
 TASK 52-13-21-820-001
　
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(132)