Airworthiness Directives (ADs)
CAA-2010-04-007A(已被CAA-2013-07-008取代)
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
- 2010/06/01
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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, A320-111,
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 aeroplanes, all manufacturer serial numbers.
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Model Number
- AIRBUS A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2010-04-007A(已被CAA-2013-07-008取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0071R1
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Effective Date
- 2010/06/11
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Subject
- Time Limits and Maintenance Checks – Damage Tolerant
Airworthiness Limitation Items – ALS Part 2 – Amendment
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Reference Publications (Revision/ATA/SB)
- ATA 05. This AD revises EASA AD 2010-0071(CAA-2010-04-007) dated 15 April 2010, which superseded EASA AD 2006-0165(CAA-2006-06-013) dated 13 June 2006. Ref. Airbus A318/A319/A320/A321 ALI Document reference AI/SE-M4/95A.0252/96 issue 10, approved by EASA on 15 March 2010 and Airbus A319 Corporate Jet ALI Document reference AI/SE-M2/95A.1038/99
issue 2, approved by EASA on 15 March 2010.
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Remarks
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