Airworthiness Directives (ADs)
CAA-2012-09-007B
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
- 2016/02/04
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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
- Airbus A318, A319, A320, A321 aeroplanes.
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CAA AD Number
- CAA-2012-09-007B
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0175R2
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Effective Date
- 2016/02/04
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Subject
- Flight Controls – Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines – Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- (i)This AD revises EASA AD 2012-0175R1(CAA-2012-09-007A). (ii) Airbus SB A320-27-1214 original issue dated 23 February 2012. Airbus SB A320-27-1222 original issue dated 17 July 2015. Goodrich SB 47145-27-16 original issue dated 07 November 2011. UTAS SB 47145-27-18 original issue dated 31 March 2015. UTAS SB 47145-27-20 original issue dated 16 July 2015. 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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