Airworthiness Directives (ADs)
CAA-2016-09-011
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
- 2016/09/19
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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-2016-09-011
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0184
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Effective Date
- 2016/09/20
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Subject
- Flight Controls – Trimmable Horizontal Stabilizer Actuator – Inspection / Replacement (Life Limitation)
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Reference Publications (Revision/ATA/SB)
- ATA 27. This AD supersedes EASA AD 2014-0011R1(CAA-2014-01-005A) dated 17 January 2014. Ref. Publications: Airbus SB A320-27-1227 original issue dated 01 July 2013, or Revision 01 dated 07 October 2013, or Revision 02 dated 02 February 2015, or Revision 03 dated 29 April 2016. UTAS SB 47145-27-19 original issue dated 15 December 2015.
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Remarks
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