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Instrument
Instrument identification
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
Applicability
All model FA-200-180 with S/No. 12 and subsequent.
Requirement
Requirement
Install new engine driven fuel pump outlet tee P/No. AN783-6.
Note
Note
Fuji SB No. 200-004 and Japanese CAB AD TCD-2213-82 refer.
Compliance
Compliance
Within 100 hours time in service after 31 March 1983 and thereafter at intervals of 3000 hours time in service.
Background
Background
Instances of fatigue cracking have been reported by the manufacturer. This AD has been amended to restrict the service life of the component.