Airworthiness Directives (ADs)
CAA-2003-12-014E(已有後續修訂版)
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2006/10/16
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Applicability
- AIRBUS A340 aircraft, models -211, -212, -213, -311, -312 and -313, all
serial numbers, except those on which AIRBUS modification 52980 has
been embodied in production or AIRBUS Service Bulletin (SB) A340-32-
4222 Revision 01 or AIRBUS SB A340-32-4213 Revision 01 has been
embodied in-service.
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Model Number
- A340-200/-300 Series Aircraft
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CAA AD Number
- CAA-2003-12-014E(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2006-0301R1
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Effective Date
- 2006/10/19
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Subject
- Landing Gear - Main Landing Gear Retraction Actuator
Piston Rod - Inspection/Modification
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Reference Publications (Revision/ATA/SB)
- ATA 32
Revision/Supersedure : This AD revises EASA AD 2006-0301 superseded DGAC AD F-2005-099(CAA-2003-12-014D).
Ref. AIRBUS SB A340-32-4212, R1, R2, R3 or R4; A340-32-4222R1; and A340-32-4213R1.
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Remarks
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