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Airworthiness Directives (ADs)

CAA-2012-09-007A(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
2014/01/13
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 and A321 aeroplanes
CAA AD Number
CAA-2012-09-007A(已有後續修訂版)
Aeronautics Authority of Original AD
EASA
Original AD Number
2012-0175R1
Effective Date
2014/01/21
Subject
Flight Controls – Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines – Inspection / Replacement
Reference Publications (Revision/ATA/SB)
ATA 27. This AD revises EASA AD 2012-0175(CAA-2012-09-007) dated 07 September 2012. Ref. Airbus SB A320-27-1214 original issue dated 23 February 2012, and Goodrich SB 47145-27-16 original issue dated 07 November 2011.
Remarks
Download
CAA-2012-09-007A.pdf
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