Airworthiness Directives (ADs)
CAA-2009-02-003(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.
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Issue Date
- 2009/02/13
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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 aircraft models, all manufacturer serial numbers.
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Model Number
- A318, A319, A320 and A321 aircraft
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CAA AD Number
- CAA-2009-02-003(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2009-0025
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Effective Date
- 2008/02/24
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Subject
- Wings – Flap Track No.1 Pendulum Assembly – Inspection /
Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 57
Ref. Publications:AIRBUS SB A320-57-1144 dated 06 February 2007, or SB A320-57-1144 Revision 1 dated 18 June 2007; AIRBUS SB A320-57A1146 dated 21 September 2007.
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Remarks
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