Commonwealth legislation

AD/FA-200/9 Amdt 1 - Engine Driven Fuel Pump Outlet Tee - Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of Fuji FA-200-180 aeroplanes (serial no. 12 and later) to install engine‑driven fuel pump outlet tee P/No. AN783‑6 within 100 hours’ flying time after 31 March 1983 and replace it every 3,000 hours thereafter. It was issued to address reported fatigue cracking; operators must arrange and pay for parts, labour and scheduling to meet the mandated intervals.

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AD/FA-200/9 Amdt 1 - Engine Driven Fuel Pump Outlet Tee - Replacement

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.