(m)
Make sure that the lockwashers (6) are correctly positioned.
(n)
Safety the nuts (5) and the lockwashers (6) with MISCELLANEOUS (Material No. 19-010).
(7) Open the door and remove the shims located between the upper fittings
(1) and the rollers (2).
R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 52-13-21Page 510 1401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C ALL
Subtask 52-13-21-820-050
B. Adjustment of the Safety Pin
(Ref. Fig. 503/TASK 52-13-21-991-002)
(1)
Close the door
(2)
Make sure that the clearance J1 between the safety pin (23) and the frame fitting (20) is 4 -1 +1 mm (0.1574 -0.0393 +0.0393 in.).
(3)
If the clearance J1 is not in the tolerance, adjust as follows:
(a)
Open the door.
(b)
Remove the screw (21) and the adjustable washer (22).
(c)
Put a new adjustable washer (22) to get the correct clearance J1.
(d)
Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-007A) on the threads of the screw (21).
(e)
Install the screw (21).
(f)
TORQUE the screw (21) to between 0.6 and 0.7 m.daN (53.09 and
61.94 lbf.in).
Subtask 52-13-21-820-054
C. Adjustment of the Proximity Switch of the Locking Hook
(1) Do an adjustment of the proximity switches (15WV1 or 15WV2) (Ref. TASK 52-71-00-820-001).
1EFF : ALL 1 52-13-21Page 511 1 1 Feb 01/01 1 1 1CES 1
Safety Pin Adjustment
Figure 503/TASK 52-13-21-991-002
1EFF : ALL 1 52-13-21 Page 512
1 1 Feb 01/01
1 1
1CES 1
5. Close-up
________ Subtask 52-13-21-410-050
A. Install of Components
(1)
Install the door insulation.
(2)
Install the door lining panels (Ref. TASK 25-23-46-400-001).
(a)
For the left passenger/crew door 832 832EZ.
(b)
For the right passenger/crew door 842 842EZ.
(3) Install the lining flap (Ref. TASK 52-11-31-400-001). Subtask 52-13-21-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
Subtask 52-13-21-410-051
C. Close Access
(1)
Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).
(2)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(3)
Close the applicable passenger/crew door 832 or 842 (Ref. TASK 52-10-00-410-001).
(4)
Remove the access platform(s).
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : ALL 1 52-13-21Page 513 1 1 Feb 01/01 1 1 1CES 1 MECHANISM - DOOR LOCKING - INSPECTION/CHECK
___________________________________________
TASK 52-13-21-220-001
Detailed Visual Inspection of the Door Locking Mechanism
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 3.50 m (11 ft. 6 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew
Door 52-10-00-915-001 Replacement of the Bushes 52-13-21-000-001 Removal of the Door Locking Mechanism 52-13-21-400-001 Installation of the Door Locking Mechanism 52-13-21-991-023 Fig. 601 52-13-21-991-024 Fig. 602 52-13-21-991-025 Fig. 603 52-13-21-991-026 Fig. 604 52-13-21-991-027 Fig. 605 52-13-21-991-028 Fig. 606 52-13-21-991-029 Fig. 607
1EFF : ALL 1 52-13-21Page 601 1 1 Feb 01/98 1 1 1CES 1
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM DOORS 舱门2(135)
