Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Enstrom F-28 Series Helicopters
AD/ENST 28/24 Main Rotor Retention Assembly - Inspection 10/82
Applicability: All model F-28A, F-28C, F-28F, 280, 280C and 280F. Document: Enstrom Service Directive Bulletin No. 0057. Note: FAA AD 82-16-09 Amdt. 39-4429 refers.
Compliance: Within 100 hours time in service after 31 October 1982, and thereafter at intervals not exceeding 200 hours time in service.
Background: Manufacture reports misalignment of the nylon shims has worn grooves in the inner surfaces of the blade grip.
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