Airworthiness Directives (ADs)
CAA-2012-07-002(已被CAA-2024-05-006取代)
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, A320-211, 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.
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Model Number
- A318, A319, A320 and A321 aeroplanes.
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CAA AD Number
- CAA-2012-07-002(已被CAA-2024-05-006取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0118
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Effective Date
- 2012/07/18
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Subject
- Fuselage – Centre Fuselage / Main Landing Gear (MLG) Door Keel Beam Hinge and Actuator Fittings – Inspection.
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Reference Publications (Revision/ATA/SB)
- (i) This AD supersedes EASA AD 2007-0161 (CAA-2007-06-008) dated 11 June 2007. (ii)Airbus SB A320-53-1195 Revision 03, dated 08 November 2011.(iii) Airbus SB A320-53-1196 Revision 02, dated 08 November 2011.(iv) Airbus A318/A319/A320/A321 ALI document reference AI/SE-4/95A.0252/96 issue 11, approved by EASA on 09 November 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
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Remarks
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