Document ID: chunk:federal_register_of_legislation:F2006B08755:body:0
Version: federal_register_of_legislation:F2006B08755
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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.