Airworthiness Directives (ADs)
CAA-2012-06-005B(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
- 2012/07/06
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Applicability
- Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers that have received AIRBUS modification (mod) 33844 (CFM56 engines), or mod 33847 (IAE V2500 engines) or mod 33687 (PW6000 engines) in production, which introduce an improved aerodynamic pylon shape.
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Model Number
- Airbus A318, A319, A320, A321 aeroplanes.
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CAA AD Number
- CAA-2012-06-005B(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0100R2
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Effective Date
- 2012/07/09
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Subject
- Nacelles/Pylons – Aft Pylon Moveable Fairing Rib 5 – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- (i) This AD revises EASA AD 2012-0100R1 dated 19 June 2012(CAA-2012-06-005A).
(ii) Airbus SB A320-54A1026 Original issue dated 19 April 2012.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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Remarks
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