Airworthiness Directives (ADs)
CAA-2020-12-015
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
- 2020/12/29
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Applicability
- AS 365 N2, AS 365 N3, SA 365 C1, SA 365 C2, SA 365 C3, SA 365 N and SA 365 N1 helicopters, all serial numbers (s/n) on which AH modification (mod) 07 63B64 has been embodied; and
EC 155 B and EC 155 B1 helicopters, all s/n.
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Model Number
- Airbus Helicopters SA 365, AS 365
and EC 155 helicopters
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CAA AD Number
- CAA-2020-12-015
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2020-0287
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Effective Date
- 2021/01/04
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Subject
- Tail Rotor Drive – Tail Rotor Drive Flange / Shaft Flexible Coupling – Inspection / Modification
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Reference Publications (Revision/ATA/SB)
- This AD supersedes EASA AD 2020-0212(CAA-2020-10-003) dated 05 October 2020.
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Remarks
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Download
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