Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 400 Series Aeroplanes
AD/CESSNA 400/70 Elevator Horn Inboard Tip Rib - Modification
Applicability: All model 441 with S/Nos. 441-0001 to -0106 and 0109. Document: Cessna Propjet SIL No. PJ79-32.
4/80 Compliance: Unless already accomplished, within 25 hours time in service after 28 February 1980.
Background: Sealing of the inboard tip rib of the elevator horn is required to preclude foreign material from entering or exiting the elevator tip rib.
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