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 210/65 Fuel Line Chafing 1/92 DM
Applicability: All Cessna 210 series with S/N 21059062 through 21064535, T210-0393 through T210-0454 and P21000001 through P21000760.
Requirement: Unless previously carried out action in accordance with Cessna Service Information Letter SE82-32. A minimum clearance of 6.5mm (0.25 inches) must be obtained between the fuel line/electrical wiring loom.
Note: FAA AD 91-22-01 Amdt 39-8061 refers.
Compliance: Within 50 hours time in service from 22 November 1991 or by 30 April 1992, whichever occurs first.
Background: Chafing of the fuel line by the wiring loom in the nose gear tunnel area could result in an inflight fire.
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