AD/DAUPHIN/44 - Tail Rotor Hub Fairing

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08755 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Eurocopter SA 360 and SA 365 (Dauphin) Series Helicopters

 

AD/DAUPHIN/44 Tail Rotor Hub Fairing  9/95 TX

 

Applicability: Model SA 365C, C1, C2, and C3, and 365N.

 

Requirement: Action in accordance with Eurocopter Telex Service No. 01.34 or 01.43 as applicable.

 

Note: DGAC ADs 95-112-040(B) and 95-107-039(B) R1 refer.

 

Compliance: Prior to further flight after 7 July 1995, thereafter in accordance with the Requirement Document.

 

Background: There have been in service reports of ruptured springs, which both DGAC and Eurocopter consider to be an urgent airworthiness matter.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.