交通部民用航空局

發布日期

2016/12/06

適用性說明

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.

型別

A318, A319, A320 and A321 aeroplanes

民航局AD編號

CAA-2016-12-002(已有後續修訂版)

原發布國

EASA

原AD編號

2016-0238

生效日期

2016/12/16

主旨摘要

Fuselage-Door Stop Fitting Holes at Frames 66/68-Inspection / Repair

參考資訊（版本/ATA/SB）

ATA 53. This AD supersedes EASA AD 2016-0015(CAA-2016-01-006) dated 15 January 2016. 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. 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. and Airbus SB A320-53-1288, original issue dated 10 October 2014, or Revision 01 dated 03 October 2016. and Airbus SB A320-53-1290, original issue dated 10 October 2014, or Revision 01 dated 03 October 2016.

存檔序號

105-12-002

專業分項

Structure

產品類別

Airplane

備註

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