Airworthiness Directives (ADs)

Aviation Industry

CAA-2014-07-023A(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.

Issue Date: 2014/08/05

Applicability: - 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 helicopters, all serial numbers (S/N), on which Airbus Helicopters modification 0763B64 has been embodied; - EC 155 B, EC 155 B1 helicopters, all S/N

Model Number: SA 365, SA 366, AS 365 and EC 155 helicopters

CAA AD Number: CAA-2014-07-023A(已有後續修訂版)

Aeronautics Authority of Original AD: EASA

Original AD Number: 2014-0179R1

Effective Date: 2014/08/01

Subject: Rotor Drive(s) – Tail Rotor Drive Flange – Inspection

Reference Publications (Revision/ATA/SB): ATA 63. This AD revises EASA AD 2014-0179(CAA-2014-07-023) dated 25 July 2014, which superseded EASA AD 2014-0165(CAA-2014-07-008) dated 14 July 2014. Ref. Airbus Helicopters ASB AS365-63.00.18 original issue, dated 09 July 2014, and 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 original issue dated 09 July 2014 or Revision 1, dated 21 July 2014.

Remarks

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