Lock Pin on the Inflation Reservoir
Figure 201/TASK 52-22-00-991-027
1EFF : 301-399, 1 52-22-00 Page 203
1 1 May 01/04
1 1
1CES 1
Normal Operation from the Passenger Compartment
Figure 202/TASK 52-22-00-991-001
1EFF : 301-399, 1 52-22-00Page 204 1 1 May 01/04 1 1 1CES 1 Subtask 52-22-00-010-051
B. Opening of the Emergency Exit Doors
(Ref. Fig. 201/TASK 52-22-00-991-027, 202/TASK 52-22-00-991-001)
(1)
Open the handle cover to get access to the inboard handle.
(2)
Pull up the inboard handle to the OPEN position so that the door lifts.
NOTE : The indication window must show UNLOCKED in red.
____
(3)
With the assist handle, push the door outboard to get access to the door damper and emergency operation cylinder.
(4)
Do the special precaution on the door damper and emergency operation cylinder (Ref. TASK 52-22-00-860-003).
(5)
Open the door so that the door stay mechanism locks the door in its fully open position.
(6)
Install the SAFETY PIN - SLIDE RELEASE LEVER (98D52207551000) in the slide release lever and the frame fitting. (Ref. Fig. 201/TASK 52-22-00-991-027)
NOTE : This prevents the accidental operation of the escape-slide
____
release mechanism.
1EFF : 301-399, 1 52-22-00Page 205 1 1 May 01/04 1 1 1CES 1 TASK 52-22-00-410-001
Closing of the Emergency Exit Doors from the Passenger Compartment
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.) 98A52107632000 1 PIN - SAFETY SLIDE 98D52207551000 1 SAFETY PIN - SLIDE RELEASE LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power 52-10-00-410-001 Closing of the Passenger/Crew Door 52-22-00-860-004 Special Precaution after Maintenance on the Door
Damper and Emergency Operation Cylinder 52-22-00-991-027 Fig. 201 52-22-00-991-001 Fig. 202
3. Job Set-up
__________
Subtask 52-22-00-860-058
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the access platform is in position below the opened door.
1EFF : 301-399, 1 52-22-00Page 206 1 1 May 01/04 1 1 1CES 1
4. Procedure
_________ Subtask 52-22-00-410-051
A. Closing of the Door
(Ref. Fig. 201/TASK 52-22-00-991-027, 202/TASK 52-22-00-991-001)
(1)
Push the release button so that the door stay mechanism releases the door.
(2)
With the assist handle, pull the door rearward until you get access to the door damper and emergency operation cylinder.
(3)
Do the special precaution on the door damper and emergency operation cylinder (Ref. TASK 52-22-00-860-004).
(4)
Remove the SAFETY PIN - SLIDE RELEASE LEVER (98D52207551000) from the slide release lever at the fuselage door frame.
(5)
Move the door rearward and inboard until it is in the correct position at the opening.
(6)
Push down the inboard handle so that the door lowers into the opening.
NOTE : The indication window must show LOCKED in green.
____
(7) Close the handle cover to prevent the accidental operation of the inboard handle.
Subtask 52-22-00-860-060
B. Arming of the Escape Slide-release Mechanism
(1)
Remove the PIN - SAFETY SLIDE (98A52107632000) from the slide control handle.
(2)
Push down the slide control handle to set the escape slide-release mechanism of the door to the ARMED mode.
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM DOORS 艙門3(52)
