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Emergency Escape Slide Release Mechanism
**ON A/C 001-002,
(Ref. Fig. 008)
R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 008A)
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Door-Damper and Emergency-Operation Cylinder
Figure 006A
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Door Suspension
Figure 007
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1 1 May 01/98
1 1
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Escape Slide Mechanism
Figure 008
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1 1 Feb 01/99
1 1
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Escape Slide/Raft Mechanism
Figure 008A
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The emergency escape slide is installed at the bottom of the door. The slide is fastened to a girt bar. This girt bar can be locked, by means of levers and fittings:
-either to the fuselage in the emergency (armed) mode
- or to the door in the normal (disarmed) mode. The emergency control handle is located far from the inner control handle. Several rods and levers connect the emergency control handle to the girt bar actuating mechanism. A cam disk and a roller connect the emergency control handle and the outer control handle. When the outer control handle is operated, the release mechanism of the emergency escape slide returns to the DISARMED position. A locking unit, connected to the locking shaft, locks the emergency escape slide release mechanism in the disarmed position when the door is not fully closed and locked. A visual indicator is installed at the forward end of the girt bar.
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PASSENGER/CREW - MAINTENANCE PRACTICES
______________________________________ TASK 52-10-00-010-001 Opening of the Passenger/Crew Door
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 3.50 m (11 ft. 6 in.) 98D52103500000 1 SAFETY PIN - SLIDE ARMING
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
Power 52-00-00-481-001 Installation of the Safety Barriers 52-10-00-991-001 Fig. 201 52-10-00-991-043 Fig. 202
3. Job Set-up
__________ Subtask 52-10-00-861-051
A. Energize the ground service network
(Ref. TASK 24-42-00-861-001)
Subtask 52-10-00-941-050
B. Get Access
(1) Put the access platform in position in front of the applicable passenger/crew door 831 or 841 or 832 or 842.
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4. Procedure
_________
Subtask 52-10-00-010-050
A. Opening of the Passenger/Crew Door
WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES.
_______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
WARNING : DO NOT OPEN OR GO NEAR PRESSURE-SEALED DOORS WHEN THE AIRCRAFT
_______ IS PRESSURIZED. A PRESSURE-SEALED DOOR THAT OPENS WHEN THE AIRCRAFT IS PRESSURIZED.
-WILL CAUSE EXPLOSIVE DECOMPRESSION.
-CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAUSE DAMAGE TO THE AIRCRAFT/EQUIPMENT.
WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE
_______
THAN 65 KNOTS.
WARNING : BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT: 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1(68)
