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Airworthiness Directives (ADs)

CAA-2019-03-016A

依據民用航空法規,航空器所有人或使用人除應遵守本國民航局所發布適航指令,亦應遵守航空器設計國之民航主管機關所通告之適航指令。

發布日期
2019/09/17
適用機型摘要
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: - A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and - A319 aeroplanes on which Airbus mod 28162, mod 28238 and mod 28342 were embodied in production.
型別
A318, A319, A320 and A321 aeroplanes
民航局AD編號
CAA-2019-03-016A
原發布國
EASA
原AD編號
2019-0067R1
生效日期
2019/09/18
主旨摘要
Fuselage – Lateral Cockpit Window Frame Upper Stiffener – Inspection
參考資訊(版本/ATA/SB)
ATA 53. This AD revises EASA AD 2019-0067(CAA-2019-03-016) dated 27 March 2019.
存檔序號
108-09-005
專業分項
Structure
產品類別
Airplane
備註
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