Document ID: chunk:federal_register_of_legislation:F2006B06878:body:0
Version: federal_register_of_legislation:F2006B06878
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Short SD3-60 Series Aeroplanes

AD/SD3-60/33 Rudder Torque Tube Fitting 8/91

 Applicability: Model SD360.
 Requirement: Action in accordance with Mandatory Shorts Service Bulletin SD360-55-17. Compliance:              As specified in the Requirement Document with a revised effective date of 8 August
            1991 for Australian registered aircraft.

            Background:  Instances have been reported where the rudder torque tube fitting at rib 1 has been subject to exfoliation corrosion. The effective date required by the UK CAA is extended by three months.