Airworthiness Directives (ADs)

Aviation Industry

CAA-2017-01-004

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: 2017/01/18

Applicability: SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers, except helicopters equipped with a tail gearbox modified in accordance with Airbus Helicopters (AH) modification (mod) 07 65B63.

Model Number: AIRBUS HELICOPTERS SA 365 helicopter

CAA AD Number: CAA-2017-01-004

Aeronautics Authority of Original AD: EASA

Original AD Number: 2017-0007

Effective Date: 2017/01/27

Subject: Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement

Reference Publications (Revision/ATA/SB): ATA 65. This AD supersedes EASA AD 2016-0097R1(CAA-2016-05-008A) dated 25 May 2016. Ref. Publications: Eurocopter AS365 SB 65.00.17 Revision 1 dated 23 February 2011. and Eurocopter SA366 SB 65.04 Revision 1 dated 23 February 2011. and Eurocopter EC155 SB 65-006 Revision 1 dated 23 February 2011. and Airbus Helicopters ASB AS365-01.00.67 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016. and Airbus Helicopters ASB SA366-01.29 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016. and Airbus Helicopters ASB EC155-04A014 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016.

Remarks

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