Document ID: chunk:federal_register_of_legislation:F2006B09944:body:0
Version: federal_register_of_legislation:F2006B09944
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Fuji FA-200 Series Aeroplanes

 AD/FA-200/9
 Amdt 1

 Engine Driven Fuel Pump Outlet Tee - Replacement

 3/83

 Applicability: All model FA-200-180 with S/No. 12 and subsequent. Requirement:  Install new engine driven fuel pump outlet tee P/No. AN783-6.
            Note: Fuji SB No. 200-004 and Japanese CAB AD TCD-2213-82 refer.

            Compliance: Within 100 hours time in service after 31 March 1983 and thereafter at intervals of 3000 hours time in service.

            Background: Instances of fatigue cracking have been reported by the manufacturer. This AD has been amended to restrict the service life of the component.