Airworthiness Directives (ADs)
CAA-2011-07-019
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
- 2011/08/01
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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 rotor hub with Part number (P/N) 365A33351100, P/N 365A33351101 or P/N 65A33351102 installed on
the 10-blade Tail Rotor Hub of 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-2011-07-019
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0144
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Effective Date
- 2011/08/09
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Subject
- Time Limits and Maintenance checks – Tail Rotor Hub (TRH) –
Inspection and Tail Rotor - Tail Rotor Hub - Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 05,64. Ref. Eurocopter EC 155 ASB 05A021 Revision 1 dated 20 July 2011 and Eurocopter AS 365 ASB 05.00.60 Revision 1 dated 20 July 2011.
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Remarks
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