Airworthiness Directives (ADs)
CAA-2013-12-015
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
- 2013/12/27
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Applicability
- Airbus 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 anufacturer serial numbers.
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Model Number
- Airbus A319, A320, A321 aeroplanes.
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CAA AD Number
- CAA-2013-12-015
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2013-0310
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Effective Date
- 2014/01/03
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Subject
- Fuselage – Tack and Rivet Holes in Fitting Brackets at Frame 50 to Frame 63 – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- Airbus SB A320-53-1257 original Issue dated 21 December 2012. Airbus SB A320-53-1261 original Issue dated 21 December 2012, or Revision 01 [to be issued]. 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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