Document ID: chunk:federal_register_of_legislation:F2006B06550:body:0
Version: federal_register_of_legislation:F2006B06550
Segment Type: other
Provision Reference: 
Character Range: 0–660

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.