Airworthiness Directives (ADs)
CAA-2012-04-012
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
- 2012/04/24
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Applicability
- ATR 42-500 aeroplanes, from Manufacturer Serial Number (MSN)671 to 815 inclusive, except MSN 811.ATR 72-212A aeroplanes, from MSN 769 to MSN 914 inclusive, except MSN 826, 905, 908 and 911.
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Model Number
- ATR 42-500 and ATR 72-212A aeroplanes
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CAA AD Number
- CAA-2012-04-012
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0064
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Effective Date
- 2012/05/04
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Subject
- Flight Controls – Rudder Tab, Rudder Pedal and Elevator Control Rods – Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- (i)This AD supersedes EASA Emergency AD 2010-0063-E dated 01 April 2010(CAA AD CAA-2010-04-003 dated 02 April 2010).(ii)SB ATR42-27-0104 original issue or revision 1, ATR42-27-0105 original issue or revision 1, ATR72-27-1065 original issue, revision 1 or revision 2, ATR72-27-1066 original issue or revision 1.The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.(iii)ATR 42/72 AMM/JIC 27-20-00 DVI 10000 and AMM/JIC 27-21-42 RAI 10000.
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Remarks
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