Airworthiness Directives (ADs)
CAA-2010-03-012A
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
- 2012/05/25
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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 models, all manufacturer serial numbers.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes.
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CAA AD Number
- CAA-2010-03-012A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0046R1
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Effective Date
- 2012/06/06
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Subject
- Flight Controls - Elevator Servo-Control Rod Eye-end - Inspection.
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Reference Publications (Revision/ATA/SB)
- (i)This AD revises EASA AD 2010-0046 (CAA-2010-03-012), which superseded EASA AD 2008-0149 (CAA-2008-08-001).(ii)Airbus AOT A320-27A1186 original issue, dated 23 June 2008.(iii)Airbus SB A320-27A1186 Revision 05, dated 10 March 2010.(iv)Goodrich SB 31075-27-21 Revision 2 dated 04 March 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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