Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
AMD Falcon 50 and 900 Series Aeroplanes
AD/AMD 50/6 Flight Control Area at Frame 25 9/93
Applicability: Model F900 with a FJC-type interior.
Model F900 with a DASSAULT AVIATION-type interior.
Requirement: Action in accordance with the technical requirements of DGAC AD 92-067-010(B).
Note: Dassault Aviation SB F900-113 and SB F900-115 refer.
Compliance: As specified in the Requirement Document with a revised effective date of 19 August 1993.
Background: Water accumulation in the underfloor area at frame 25 would create the possibility that the engine and flight controls could jam in the event of extreme low temperature conditions. This Directive requires certain actions and checks of the water system, and a modification which is designed to improve underfloor heating.
s
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