交通部民用航空局

發布日期

2018/12/06

適用性說明

Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132 and A319-133, aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 161306 has been embodied in production, and except A319 CJ aeroplanes that have not embodied Airbus mod 160001 in production, and Airbus Service Bulletin (SB) A320-57-1193 (mod 160080) in service. Airbus 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 those on which Airbus mod 161271 has been embodied in production.

型別

A319, A320 and A321 aeroplanes

民航局AD編號

CAA-2018-10-021A(已被CAA-2022-06-016取代)

原發布國

EASA

原AD編號

2018-0233R1

生效日期

2018/12/05

主旨摘要

Fuselage – Cargo Compartment Fitting Brackets, Tack and Rivet Holes – Inspection / Repair

參考資訊（版本/ATA/SB）

ATA 53. This AD revises EASA AD 2018-0233(CAA-2018-10-021) dated 26 October 2018, which superseded EASA AD 2013-0310(CAA-2013-12-015) dated 20 December 2013. Ref. Publications: Airbus SB A320-53-1257 original issue dated 21 December 2012, or Rev. 01 dated 28 April 2016, or Rev. 02 dated 29 November 2016. and Airbus SB A320-53-1261 original issue dated 21 December 2012, or Rev. 01 dated 30 June 2015, or Rev. 02 dated 01 March 2016, or Rev. 03 dated 08 August 2016, or Rev. 04 dated 03 May 2017. and Airbus SB A320-53-1360 original issue dated 01 December 2016, or Rev. 01 dated 01 March 2018. and Airbus SB A320-53-1364 original issue dated 04 May 2018. Airbus SB A320-53-1365 original issue dated 17 April 2018.

存檔序號

107-11-018

專業分項

Structure

產品類別

Airplane

備註

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