(d)
 Install the rear inside fairing in the applicable overhead stowage compartment.

 (e)
 Close the access door of the applicable overhead stowage compartment.

 (4) Make sure that the handle cover is over the inboard handle.
 5. Close-up
________ Subtask 52-22-00-010-058
 A. Close Access
 (1)
 Close the applicable passenger/crew door (Ref. TASK 52-10-00-410-001).

 (2)
 Remove the access platform(s).

 1EFF : 301-399, 1 52-22-00Page 215 1 1 May 01/04 1 1 1CES 1 TASK 52-22-00-860-003

 Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.20 m (10 ft. 6 in.) 701-2978000 1 PIN - RIGGING 98A52107632000 1 PIN - SAFETY SLIDE
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-22-00-010-001  Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-991-003 Fig. 204
 3. Job Set-up
__________ Subtask 52-22-00-860-075
 A. Aircraft Maintenance Configuration
 (1) Make sure that the slide control handle (1) is pulled up and the PIN-SAFETY SLIDE (98A52107632000) (3) is installed.
 NOTE : In the indication window (2) the 'DISARMED' sign is in view.
____
 (2)
 Make sure that the applicable emergency exit door is partly opened to get access to the door damper (Ref. TASK 52-22-00-010-001).

 (3)
 Make sure that the access platform is in position below the applicable emergency exit door.

 1EFF : 301-399, 1 52-22-00Page 216 1 1 May 01/04 1 1 1CES 1

 4. Procedure
_________ Subtask 52-22-00-860-076
 A. Disarming of the Door Damper
 (Ref. Fig. 204/TASK 52-22-00-991-003)

 (1)
 Install the PIN - RIGGING (701-2978000) (12) on the percussion housing (13) to block the percussion mechanism of the door damper.

 (2)
 Remove and discard the lockwire from the pin of the release lever

 (11) and the knurled screw (15).

 (3)
 Loosen the knurled screw (15) so that the release lever (11) is moveable.

 (4)
 Move the release lever (11) so that it does not engage with the percussion striker (14).

 (5)
 Tighten the knurled screw (15).

 1EFF : 301-399, 1 52-22-00Page 217 1 1 May 01/04 1 1 1CES 1

 Special Precaution Procedure on the Door Damper and Emergency Operation
 Cylinder
 Figure 204/TASK 52-22-00-991-003

 1EFF : 301-399, 1 52-22-00Page 218 1 1 May 01/04 1 1 1CES 1 TASK 52-22-00-860-004

 Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.20 m (10 ft. 6 in.) 701-2978000 1 PIN - RIGGING 98A52107632000 1 PIN - SAFETY SLIDE
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-22-00-010-001  Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-991-003 Fig. 204
 1EFF : 301-399, 1 52-22-00Page 219 1 1 May 01/04 1 1 1CES 1

 3. Job Set-up
__________ Subtask 52-22-00-860-077
 A. Aircraft Maintenance Configuration
 (1) Make sure that the slide control handle (1) is pulled up and the PIN-SAFETY SLIDE (98A52107632000) (3) is installed.
　
中國航空網(wǎng) m.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3(55)