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.