Airworthiness Directives (ADs)
CAA-2010-10-008
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
- 2010/10/18
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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 aeroplane models, all serial numbers that have received Airbus modification (mod.) 26495 in production or Airbus Service Bulletin (SB) A320-27-1117 in service, except those having received Airbus mod. 38211 or mod. 150004 in production.
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Model Number
- AIRBUS A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2010-10-008
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0209
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Effective Date
- 2010/10/28
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Subject
- Flight Controls / Wings – Inboard Flap Trunnion and Sliding Panel
– Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 27/57. This AD supersedes DGAC France AD F-2005-139(CAA-2005-08-003) dated 03 August 2005, approved under EASA reference No 2005-6114. Ref. Airbus SB A320-57-1133 Revision 03, Revision 04 or Revision 05 and Airbus SB A320-57-1147 at original issue, Revision 01 or Revision 02 or Revision 03 and Airbus SB A320-57-1158 at original issue.
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Remarks
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