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Airworthiness Directives (ADs)

CAA-2012-04-014

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
2012/04/30
Applicability
Eurocopter SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers, if equipped with tail rotor blades Part number (P/N) 365A33-2131 all dash numbers, P/N 365A12-0010 all dash numbers or P/N 365A12-0020 all dash numbers.
Model Number
Eurocopter AS 365 N1, AS 365 N2 and AS 365 N3 helicopters.
CAA AD Number
CAA-2012-04-014
Aeronautics Authority of Original AD
EASA
Original AD Number
2012-0067
Effective Date
2012/05/08
Subject
Tail Rotor – Tail Rotor Blade Monitoring and Limitations.
Reference Publications (Revision/ATA/SB)
(i) This AD supersedes DGAC France AD F-2004-116 (EASA approval 2004-7515) dated 21 July 2004.(ii) Eurocopter AS 365 ASB No. 05.00.17 Revision 2 dated 16 April 2012. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Remarks
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CAA-2012-04-014.pdf
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