Federal Register of Legislation
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.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate