(4)
 Loosen the filling valve nut (3) to open the pressure filling valve (2).

 (5)
 Fill the pressure accumulator (5) with the correct pressure as follows:

 (a)
 Carefully open the control valve of the filling system and close it when the pressure gage (4) shows 55 bar (797.7073 psi).

 (b)
 After 3 sec. open the control valve again and close it when the pressure gage (4) shows 83 bar (1203.8129 psi).

 (c)
 After 3 sec. open the control valve again and close it when the pressure gage (4) shows 123 bar (1783.9637 psi).

 NOTE : The power accumulator (5) is correctly pressurized when
____ the pointer of the pressure gage (4) is in the green area (121 bar (1754.9561 psi) and 125 bar (1812.9712 psi)).
 (6)
 TORQUE the filling valve nut (3) to 1.0 m.daN (88.49 lbf.in) when the pointer of the pressure gage (4) is in the green area and stable.

 (7)
 Close the control valve of the filling system.

 (8)
 Remove the extension adapter from the pressure filling valve (2).

 (9)
 Remove the WRENCH - EMERGENCY EXIT DOOR DAMPER (7) from the filling valve nut (3).

 1EFF : 301-399, 1 52-22-00Page 304 1 1 May 01/04 1 1 1CES 1

 (10) Install the yellow protection cap (6) on the pressure filling valve

 (2).
 5. Close-up
________ Subtask 52-22-00-410-061
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the door (Ref. TASK 52-22-00-410-001).

 (3) Remove the access platform(s). Subtask 52-22-00-865-061
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 360RH6, 360RH8
 49VU COM/CIDS/DEU B/ESS 153RH G03
 Subtask 52-22-00-860-080
 C. Put the aircraft back to the serviceable condition.
 (1)
 Do the special precaution procedure on the door damper and emergency operation cylinder (Ref. TASK 52-22-00-860-004).

 (2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002)

 1EFF : 301-399, 1 52-22-00Page 305 1 1 May 01/04 1 1 1CES 1 PASSENGER COMPARTMENT EMERGENCY EXIT ((DOORS)) - ADJUSTMENT/TEST

________________________________________________________________
 **ON A/C 301-399,
 TASK 52-22-00-710-001
 Operational Check of Door Locking /Unlocking and Opening/Closing from Inside and Outside with Door Latching/Unlatching and Functional Check of Hand Force
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 522200-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific dynamometer of 20.0 daN (44.96117 lbf.) No specific access platform 3.20 m (10 ft. 6 in.) 98A52107632000 1 PIN - SAFETY SLIDE
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-22-00-010-001 Opening of the Emergency Exit Doors from the
 Passenger Compartment 52-22-00-410-001 Closing of the Emergency Exit Doors from the Passenger Compartment 52-22-00-860-003 Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder 52-22-00-860-004 Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder 52-22-00-991-020 Fig. 501
R 1EFF : 102-149, 201-207, 211-299, 301-399, 1 52-22-00Page 501 1401-499, 1Aug 01/05 1 1 1CES 1R 3. Job Set-up

__________ R Subtask 52-22-00-010-061 R A. Get Access R (1) Put the access platform in position below the applicable emergency
R exit door (referred to as door).
R (2) Open the applicable passenger/crew door (Ref. TASK 52-10-00-010-001).
R 4. Procedure

_________
R Subtask 52-22-00-710-050
R A. Operational Test of the Door Mechanism from the Inner Side R (Ref. Fig. 501/TASK 52-22-00-991-020)
R -------------------------------------------------------------------------------R ACTION RESULT R -------------------------------------------------------------------------------
　
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3(61)