Airworthiness Directives (ADs)
CAA-2016-10-006修訂(已被CAA-2024-03-010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
- 2016/10/19
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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 (MSN), except those having Airbus modification (mod) 151574 embodied in production.
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Model Number
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2016-10-006修訂(已被CAA-2024-03-010取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0206Correction
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Effective Date
- 2016/10/27
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Subject
- Fuselage – Pressure Panel Longitudinal Beams – Inspection / Repair / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 53. This AD supersedes DGAC France AD 2000-531-155(B) CAA (90-A320-148) dated 06 January 2001. Ref. Publications: Airbus SB A320-53-1029 original issue dated 05 January 2000, or Revision 01 dated 29 April 2002. and Airbus SB A320-53-1030 original issue dated 05 January 2000, or Revision 01 dated 21 May 2002. and Airbus SB A320-53-1240 original issue dated 19 March 2015, or Revision 01 dated 04 April 2016. and Airbus SB A320-53-1263 original issue dated 19 March 2015, or Revision 01 dated 29 February 2016. and Airbus SB A320-53-1264 original issue dated 19 March 2015, or Revision 01 dated 04 July 2016.
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Remarks
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