Subtask 52-00-00-081-051
B. Not Applicable
**ON A/C 301-399,
Subtask 52-00-00-081-051-A
B. Removal of the Safety Barriers from the Emergency Exit Door Frame
(1) Remove the SAFETY BARRIER - EMERGENCY EXIT DOORS (98D52003004001) from the door frame.
**ON A/C ALL
5. Close-up
________
Subtask 52-00-00-410-050
A. Close the Passenger/Crew Doors
(1)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2)
Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).
(3)
Close the applicable passenger/crew door 831 or 841 or 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.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 52-00-00-410-051
B. Not Applicable
1EFF : ALL 1 52-00-00Page 205 1 1 Aug 01/05 1 1 1CES 1 1EFF : 301-399, 1 52-00-00Page 206 1 1 May 01/04 1 1 1CES 1 PASSENGER/CREW - DESCRIPTION AND OPERATION
R **ON A/C 301-399,
R Subtask 52-00-00-410-051-A
R B. Close the Emergency Exit Doors
R (1) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R (2) Obey the special precautions after the work on the door (Ref. TASK
R 52-22-00-860-004).
R (3) Close the applicable emergency exit door 833 or 834 or 843 or 844
R (Ref. TASK 52-22-00-410-002).
R (4) Remove the access platform(s).
R (5) Make sure that the work area is clean and clear of tool(s) and other
R items.
__________________________________________
1. General
_______
A. Door Description The aircraft is provided with four type 1 passenger/crew doors, two on the left side of the fuselage and two on the right side. (Ref. Fig. 001) The doors are of fail-safe plug-type construction. During the unlocking phase the doors move inwards then upwards, they open outwards and move forwards parallel to the fuselage. All the doors include an evacuation system. The escape slides or slides/raft are stowed in hard containers at the lower part of passenger/crew door.
**ON A/C 001-002,
(Ref. Fig. 002)
R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 002A)
**ON A/C ALL
Each passenger/crew door has a locking mechanism and an escape slide or slide/raft release mechanism. The locking mechanism is controlled either with the inner or the outer control handle. The escape slide or slide/raft is controlled by an arming/disarming lever on the inner side. When the door is opened from the outside the escape slide or slide/raft release mechanism is disarmed automatically. Because all type 1 doors are similar, except for their geometry, this description is general and valid for all doors.
B. Location of Component
(1) FWD Passenger Crew/Door The main components of the FWD passenger/crew door are:
-
the door structure (Ref. 52-11-11),
-
the door suspension (Ref. 52-11-12),
-
the door seal (Ref 52-11-18),
-
the door damper and emergency-operation cylinder (Ref. 52-11-14),
-
the door locking mechanism (Ref. 52-11-21).
1EFF : ALL 1 52-10-00Page 1 1 1 Aug 01/05 1 1 1CES 1
Location of the FWD and Aft Passenger/Crew Doors
Figure 001
1EFF : ALL 1 52-10-00 Page 2
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1(66)
