Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Eagle X-TS Series Aeroplanes
AD/X-TS/3 Canard Rear Spar Reinforcement 2/2000 TX
Applicability: Models X-TS 150 and 150B serial numbers 001 to 003 and 005 to 030 inclusive. Requirement: Modify the canard rear spar bracket in accordance with Eagle Service Bulletin 1074. Compliance: Within 100 hours time in service after the effective date of this directive. This Airworthiness Directive becomes effective on 24 December 1999.
Background: This Directive is issued to provide additional strength to the canard rear spar bracket, to enable the aircraft to meet certification requirements.
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