Airworthiness Directives (ADs)
CAA-2016-12-002修訂
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
- 2017/01/10
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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, A320-211, 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, except: - aeroplanes on which Airbus modification (mod) 157039 has been embodied in production;
- A319 aeroplanes on which mod 28238, mod 28162 and mod 28342 have been embodied in production; and - A318 aeroplanes on which mod 39195 has been embodied in production or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service.
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Model Number
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2016-12-002修訂
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0238Correction
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Effective Date
- 2016/12/16
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Subject
- Fuselage – Door Stop Fitting Holes at Frames 66/68 – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- ATA 53. This AD supersedes EASA AD 2016-0015(CAA-2016-01-006) dated 15 January Ref. Publications: Airbus SB A320-57-1193, original issue dated 16 October 2015, or Revision 01 dated 05 February 2016, or Revision 02 dated 18 May 2016, or Revision 03 dated 03 August 2016, or Revision 04 dated 30 September 2016. and Airbus SB A320-53-1288, original issue dated 10 October 2014, or Revision 01 dated 03 October 2016.
Airbus SB A320-53-1290, original issue dated 10 October 2014, or Revision 01 dated 03 October 2016.
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Remarks
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