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Airworthiness Directives (ADs)

CAA-2013-12-014(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.

Issue Date
2013/12/27
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.
Model Number
Airbus A318, A319, A320, A321 aeroplanes.
CAA AD Number
CAA-2013-12-014(已有後續修訂版)
Aeronautics Authority of Original AD
EASA
Original AD Number
2013-0309
Effective Date
2014/01/03
Subject
Flight Controls – Elevator Servo-Control Rod Eye-Ends –Inspection / Replacement
Reference Publications (Revision/ATA/SB)
(i) This AD supersedes EASA AD 2010-0046R1(CAA-2010-03-012A). (ii) Airbus All Operators Telex (AOT) A320-27A1186 at original issue. Airbus SB A320-27A1186 Revision 05 dated 10 March 2010. Airbus SB A320-27-1223 original issue dated 03 September 2013. Goodrich SB 31075-27-21 Revision 2 dated 04 March 2010. Goodrich SB 31075-27-22 original issue dated 02 July 2013. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Remarks
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CAA-2013-12-014.pdf
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