Airworthiness Directives (ADs)
CAA-2012-11-003修訂(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.
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Issue Date
- 2012/11/14
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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, 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-2012-11-003修訂(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0236Correction
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Effective Date
- 2012/11/23
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Subject
- Navigation – Angle of Attack (AoA) Sensors – Replacement / Modification
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Reference Publications (Revision/ATA/SB)
- (i) This AD corrects EASA AD 2012-0236 (CAA-2012-11-003) and supersedes EASA AD 2011-0203 (CAA-2011-10-010). (ii) Airbus SB A320-34-1452 original issue dated 29 January 2010. Airbus SB A320-34-1521 original issue dated 07 May 2012, or Revision 01 dated 12 September 2012. Airbus SB A320-34-1444 original issue dated 07 October 2009. Thales SB C16291A-34-007 Revision 01 dated 03 December 2009, or Revision 02 dated 16 December 2011, or Revision 03 dated 10 April 2012, or Revision 04 dated 11 October 2012. Thales SB C16291A-34-009 original issue dated 10 September 2009, or Revision 01 dated 07 January 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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