Airworthiness Directives (ADs)
CAA-2020-10-003(已被CAA-2020-12-015取代)
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
- 2020/10/07
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Applicability
- Airbus SA 365 C1, SA 365 C2, SA 365 C3, SA 365 N and SA 365 N1 and helicopters, all serial numbers (s/n), on which Airbus Helicopters modification (mod) 07 63B64 has been embodied. and AS 365 N2 and AS 365 N3 helicopters, all s/n, on which AH mod 07 63B64 has been embodied, and which were first delivered after manufacture before 09 July 2014. and EC 155 B and EC 155 B1 helicopters, all s/n, which were first delivered after manufacture before 09 July 2014.
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Model Number
- Airbus SA 365, AS 365 and EC 155 helicopters
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CAA AD Number
- CAA-2020-10-003(已被CAA-2020-12-015取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2020-0212
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Effective Date
- 2020/10/19
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Subject
- Rotor Drive(s) – Tail Rotor Drive Flange – Inspection / Modification
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Reference Publications (Revision/ATA/SB)
- This AD supersedes EASA AD 2014-0179R2(CAA-2014-07-023B) dated 11 April 2016 and EASA AD 2019-0046(CAA-2019-03-006) dated 11 March 2019.
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Remarks
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