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.