Airworthiness Directives (ADs)
CAA-2012-10-015(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
- 2012/10/31
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Applicability
- Eurocopter EC 155 B, EC 155 B1, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers, if equipped with a 10-blade Tail Rotor Hub (TRH) with Part number (P/N) 365A33351100, P/N 365A33351101 or P/N 365A33351102 installed on the quiet fenestron tail rotor; and Eurocopter AS 365 N3 helicopters, all serial numbers, if equipped with an 11-blade TRH with P/N 365A33216001 or P/N 365A33216003 installed on the quiet fenestron tail rotor.
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Model Number
- Eurocopter EC 155, SA 365 and AS 365 Helicopters
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CAA AD Number
- CAA-2012-10-015(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0227
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Effective Date
- 2012/11/07
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Subject
- Tail Rotor – Tail Rotor Hub – Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- (i) This AD supersedes EASA AD 2011-0144(CAA-2011-07-019). (ii)Eurocopter EC 155 ASB 05A021 Revision 1 dated 20 July 2011. Eurocopter ASB AS365-05.00.60 Revision 2 dated 09 October 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
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Remarks
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