Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Airbus Industrie A319, A320 and A321 Series Aeroplanes
AD/A320/55 Centre Wing, Bracket Between Shroud Box and Fixed Shroud
Applicability: As specified in the Requirement Document.
Requirement: Action in accordance with Airbus Industrie SB A320-57-1034 Rev. 1.
Note: DGAC AD 95-100-068(B) refers.
9/95
Compliance: Prior to attaining 17 000 flight cycles, thereafter at the intervals specified in the Requirement Document.
Note: Full incorporation of Airbus Industrie SB A320-57-1035 terminates this Directive.
Background: This Directive is issued to detect and/or prevent any damage related to structural fatigue.
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