Airworthiness Directives (ADs)
CAA-2014-07-023B
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
- 2016/04/14
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Applicability
- SA 365 C, SA 365 C1, SA 365 C2, SA 365 C3, SA 365 N, SA 365 N1 and SA 366 G1 helicopters, all serial numbers, on which Airbus Helicopters modification (mod) 0763B64 has been embodied. and AS 365 N3 and AS 365 N2 helicopters, all serial numbers on which Airbus Helicopters mod 0763B64 has been embodied and first delivered after manufacture before 09 July 2014.
EC 155 B and EC 155 B1 helicopters, all serial numbers first delivered after manufacture before 09 July 2014.
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Model Number
- SA 365, SA 366, AS 365 and EC 155 helicopters
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CAA AD Number
- CAA-2014-07-023B
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0179R2
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Effective Date
- 2016/04/11
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Subject
- Rotor Drive(s) – Tail Rotor Drive Flange – Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 63. Ref. Publications: Airbus Helicopters ASB AS365-63.00.18 original issue dated 09 July 2014, or Revision 1 dated 07 March 2016.
Airbus Helicopters ASB SA365-65.50 original issue dated 09 July 2014. and Airbus Helicopters ASB SA366-63.09 original issue dated 09 July 2014. and Airbus Helicopters ASB EC155-63A012 Revision 1 dated 21 July 2014, or Revision 2 dated 07 March 2016.
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Remarks
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