Airworthiness Directives (ADs)
CAA-2013-06-003(已被CAA-2018-04-003取代)
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
- 2013/06/10
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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 (MSN).
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Model Number
- AIRBUS A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2013-06-003(已被CAA-2018-04-003取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2013-0122
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Effective Date
- 2013/06/19
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Subject
- Fuselage – Belly Fairing and Keel Beam Side Panel Attachment Angles – Inspection / Replacement / Repair
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Reference Publications (Revision/ATA/SB)
- ATA 53. This AD supersedes DGAC France AD 92-201-030(CAA:81-A320-008) dated 30 September 1992. Ref. Airbus SB A320-53-1014 original issue dated 25 June 1992, or Revision 01, dated 26 May 1993, or Revision 02, dated 01 September 1994, and Airbus SB A320-53-1259 original issue, dated 06 November 2012.
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Remarks
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