Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Rolls Royce Turbine Engines - RB211 Series
AD/RB211/2 H.P. Compressor Stage 1 and 2 Disc - Removal 1/82
Applicability: RB211-22B-02, 524-02, 524B-02, 524B2-19, 524B2-39, 524B3-02 and 524C2-19 incorporating HP compressor stage 1 and 2 disc assemblies specified in Alert SB RB211-72-A5885, Rev. 2.
Document: Rolls Royce RB211 SB RB211-72-A5885, Rev. 2. Compliance: In accordance with the requirement document. Background: Removal of suspect discs is necessary to prevent uncontained failures.
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