B. Consumable Materials
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REFERENCE DESIGNATION
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No specific lockwire, corrosion-resistance steel, dia 0.8 mm
(0.032 in.)
C. Referenced Information
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REFERENCE DESIGNATION
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25-23-47-000-004 Removal of the Door Frame Linings of the LH FWD Emergency Exit Door, zone 231 25-23-47-000-009 Removal of the Door Frame Linings of the RH FWD Emergency Exit Door, zone 232 25-23-47-400-004 Installation of the Door Frame Linings of the LH FWD Emergency Exit Door, zone 231 25-23-47-400-009 Installation of the Door Frame Linings of the RH FWD Emergency Exit Door, zone 232
R 1EFF : 102-149, 201-207, 211-299, 301-399, 1 52-22-00Page 509 1401-499, 1Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
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25-23-47-400-010 Installation of the Door Frame Linings of the LH/RH
AFT Emergency Exit Doors, zones 251/252. 25-24-41-000-001 Removal of the Overhead Stowage Compartments 25-24-41-400-001 Installation of the Overhead Stowage Compartments 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
**ON A/C 301-399,
52-22-00-991-025 Fig. 502
52-22-00-991-028 Fig. 503
R **ON A/C 102-149, 201-207, 211-299, 301-399, 401-499,
3. Job Set-up
__________
**ON A/C 301-399,
Subtask 52-22-00-010-070
A. Get Access
(1)
Open the access door of the overhead stowage compartment above the applicable emergency exit door (referred to as door).
(2)
Loosen the quick-release fasteners and remove the rear inside fairing of the applicable overhead stowage compartment.
(3)
If necessary, remove the overhead stowage compartment (Ref. TASK 25-24-41-000-001) and/or the related door frame linings (Ref. TASK 25-23-47-000-004), (Ref. TASK 25-23-47-000-009) and (Ref. TASK 25-23-47-400-010) to get sufficent clearance.
R 1EFF : 102-149, 201-207, 211-299, 301-399, 1 52-22-00Page 510 1401-499, 1Aug 01/05 1 1 1CES 1 1EFF : 102-149, 201-207, 211-299, 301-399, 1 52-22-00Page 511 1 1 May 01/04 1 1 1CES 1
R Subtask 52-22-00-860-072
R B. Aircraft Maintenance Configuration
R (Ref. Fig. 502/TASK 52-22-00-991-025)
R (1) Install the lock pin on the operation valve of the inflation
R reservoir to prevent an accidental operation
R (2) Disconnect the inflation reservoir from the release lever as follos:
R (a) Remove the lockwire and open the safety clamp on the release
R lever.
R (b) Remove the release cable from the release lever.
R (3) Make a mark to identify the start position of the bellcrank lever.
R (4) Make sur that the special precaution on the door damper and emergency
R operation cylinder are done (Ref. TASK 52-22-00-860-003).
R **ON A/C 102-149, 201-207, 211-299, 301-399,
4. Procedure_________
R **ON A/C 301-399,
R Subtask 52-22-00-710-054
R A. Operational Test of Door Unlocking from Inside/Outside in "Armed"
R Position
R (1) Make sure that the applicable door is closed and locked and the slide
R control handle is in the ARMED position (Ref. TASK 52-22-00-410-001).
R Measurement of Actuation Travel
R Figure 502/TASK 52-22-00-991-025- 12 (SHEET 1)
1EFF : 301-399, 1 52-22-00Page 512 1 1 May 01/04 1 1 1CES 1 中國航空網 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(64)
