Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 210 Series Aeroplanes
AD/CESSNA 210/46 Turbocharger - Inspection 6/80
Applicability: Model T210 S/Nos. T210-0001 thru T210-0454. Model 210 S/Nos. 21058140, 21059200 thru 21063954.
Document: 1. Cessna SIL No. SE 80-24; or
2. FAA AD 80-07-01, Amdt. 39-3719.
Compliance: Within 100 hours time in service after 30 June 1980.
Background: This Directive is issued to preclude a failure of the turbocharger anti-rotation pin and its ingestion into the scavenge pump. This in turn could cause a failure of the pressure and scavenge pumps.
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