Airworthiness Directives (ADs)
CAA-2012-10-015A
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
- 2018/03/12
-
Applicability
- EC 155 B, EC 155 B1, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all manufacturer serial numbers (MSN), 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, except helicopters modified in production in accordance with Airbus Helicopters (AH) modification (mod) 0764B51; and
AS 365 N3 helicopters, all MSN, if equipped with an 11-blade TRH with P/N 365A33216001 or P/N 365A33216003 installed on the quiet fenestron tail rotor.
-
Model Number
- AIRBUS EC 155, SA 365 and AS 365 helicopters
-
CAA AD Number
- CAA-2012-10-015A
-
Aeronautics Authority of Original AD
- EASA
-
Original AD Number
- 2012-0227R1
-
Effective Date
- 2018/03/08
-
Subject
- Tail Rotor – Tail Rotor Hub – Inspection / Replacement
-
Reference Publications (Revision/ATA/SB)
- ATA 64. This AD revises EASA AD 2012-0227(CAA-2012-10-015) dated 29 October 2012, which superseded EASA AD 2011-0144 dated 26 July 2011. Ref. Publications: Eurocopter ASB AS365-05.00.60 Revision 2 dated 09 October 2012. and AH Service Bulletin AS365-64.00.30 original issue dated 13 February 2018.
-
Remarks
-
Download
-
