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-200/20 Fuselage Rear Bulkhead - Inspection 2/83
Applicability: All models with S/Nos. up to and including S/N 296. Document: Fuji Service Bulletin No. FAS 200-003. Compliance: Within the next 100 hours time in service and thereafter at intervals not exceeding 100 hours time in service, until modified in accordance with SB FAS 200-003.
Background: Cracks have been found in the upper corners of the fuselage bulkhead at F.S. 7105, near the horizontal stabiliser main spar attachment.
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