Airworthiness Directives (ADs)
CAA-2014-07-023(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
- 2014/08/05
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Applicability
- Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale). SA 365 C,SA 365 C1, SA 365 C2, SA 365 C3, SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B, EC 155 B1 helicopters, all serial numbers.
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Model Number
- Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale). SA365, AS365, SA366, EC155 helicopters.
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CAA AD Number
- CAA-2014-07-023(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0179
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Effective Date
- 2014/08/01
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Subject
- Rotor Drive(s) – Tail Rotor Drive Flange – Inspection
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Reference Publications (Revision/ATA/SB)
- (i) This AD supersedes EASA AD 2014-0165 (CAA-2014-07-008). (ii) Airbus Helicopters ASB AS365-63.00.18 original issue, dated 09 July 2014, Airbus Helicopters ASB SA365-65.50 original issue, dated 09 July 2014, Airbus Helicopters ASB SA366-63.09 original issue, dated 09 July 2014, Airbus Helicopters ASB EC155-63A012 original issue, dated 09 July 2014. 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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