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

 Eurocopter SA341 and SA342 (Gazelle) Series Helicopters

                     AD/GAZELLE/9  Main Gearbox Input Gear Flange - Inspection of Attachment Nut

5/80

            Applicability: Models SA-341 and SA-342 fitted with main gearbox P/N 341A.32.1000.01 to .05, not modified in accordance with AMS 07.7076/S374.

 Document: Gazelle SB 65.19.

 Compliance: Within 100 hours time in service after 30 June 1980.

            Background: The manufacturer has introduced an inspection to ensure that the correct torque load has been applied to the notched nut which retains the input gear flange.