Cowl Swirl Anti-Ice System
Figure 004
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Access Panels on Air Intake Cowl
Figure 005
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E E Feb 01/98 E E ECES E The acoustic panels are structural and, as such, carry air intake cowl loads. The intake cowl aft bulkhead forms a land for the fan cowl leading edge.
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F. Air Intake Cowl Materials The intake cowl structural assembly is a combination of composite skin, bonded sandwich acoustic structure and riveted conventional sheet metal structure. See following table for component materials.
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Inner barrel 2024 aluminium skins 5052 aluminium honeycomb core/ HFT non metallic core
Outer barrel graphite epoxy composite skins aluminium access panel
Lip assembly 2219 aluminium skin titanium 6-4 bulkhead
Aft bulkhead titanium 6-4 web and stiffeners titanium 6-4 inner cap 2024 aluminium outer cap
Engine attachment titanium 6-4 forged ring
G. Air intake cowl Removal/Installation (Ref. Fig. 006)
An alignment pin installed on the inlet cowl attachment ring provides an aid to installation.
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Alignment Pin
Figure 006
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AIR INTAKE COWL - REMOVAL/INSTALLATION
______________________________________ TASK 71-11-00-000-041 Removal of the Air Intake Cowl
1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific protective covers No specific universal attach pads No specific warning notice No specific access platform 1 m (3 ft. 3 in.) RSE1112 1 SLING - AIR INTAKE COWL RSE1116 1 DOLLY - AIR INTAKE COWL
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
30-21-51-000-041 Removal of the Engine Air Intake Anti-ice Valve
(4000DN) 71-13-00-010-040 Opening of the Fan Cowl Doors 71-11-00-991-300 Fig. 401
3. Job Set-up
__________ Subtask 71-11-00-941-050
A. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a warning notice to tell persons not to start the engine.
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(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC 1(2).
Subtask 71-11-00-010-050
B. Get Access
(1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
(2) Put the access platform in position.
4. Procedure
_________ (Ref. Fig. 401/TASK 71-11-00-991-300) Subtask 71-11-00-020-056
A. Removal of the Hardware
(1) Disconnect the electrical connector (45) for the interphone jack (4001VC-A) from the fan case receptacle.
(2) Install the protective covers on the electrical connector and the receptacle.
(3) Remove the anti-ice valve (40) (Ref. TASK 30-21-51-000-041).
(4) Remove the clamps (30) and the preformed hose (35) that attach the ECU and the ECU cooling air duct. 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 動力裝置 POWER PLANT 1(91)
