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Airworthiness Directives (ADs)

CAA-2011-08-013A(已有後續修訂版)

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.

Issue Date
2011/11/18
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, A320-111, 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 aeroplane models, all manufacturer serial numbers
Model Number
AIRBUS A318, A319, A320 and A321 aeroplanes
CAA AD Number
CAA-2011-08-013A(已有後續修訂版)
Aeronautics Authority of Original AD
EASA
Original AD Number
2011-0155R1
Effective Date
2011/11/29
Subject
Time Limits and Maintenance Checks – Fuel Airworthiness Limitations – ALS Part 5 – Amendment
Reference Publications (Revision/ATA/SB)
ATA 05. This AD revises EASA AD 2011-0155(CAA-2011-08-013) dated 25 August 2011, which superseded EASA AD 2006-0203 dated 11 July 2006. Ref. AIRBUS A318/A319/A320/A321 FAL Document reference 95A.1931/05 issue 4, approved by EASA on 26 August 2010.
Remarks
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