Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 99 Series Aeroplanes
AD/BEECH 99/6 Wing Structural Fatigue Limitations 12/96
Applicability: All model 99 aircraft.
Requirement: Inspect and retire the wing structural components in accordance with the Beechcraft 99 Airliner Series Continued Airworthiness Program Inspection Manual P/N 98- 30131 Rev. A1, Sections 57-10 and 57-20.
Note: FAA AD 92-15-13 refers.
Compliance: This Directive takes effect 7 November 1996.
Background: This Directive requires life limited components to be retired to prevent fatigue failure of the wing spar and associated structure.
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