Document ID: chunk:federal_register_of_legislation:F2006B06679:body:0
Version: federal_register_of_legislation:F2006B06679
Segment Type: other
Provision Reference: 
Character Range: 0–971

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Rolls Royce Turbine Engines - Spey Series

AD/RRT-S/10 HP2 Turbine Disc Locating Sleeve 13/87 DM

            Applicability: Spey 506-14, 506-14A, 506-14D, 511-5W, 511-8, 511-14, 511-14W, 512-14DW, 512-14E, 555-15, 555-15H, 555-15N, 555-15P.

 Requirement: Action in accordance with the Requirements of Rolls Royce SB Sp 72-932 Rev 1.

            Note: Reference Documents:

              1. Fokker SB F28/72-6.

2.    Netherlands AD Fokker F28 BLA nr. 87-62. Compliance: In accordance with the Requirement Document.
            Background: This Directive has been issued to require HP turbine stage 2 disc retaining sleeves to be replaced at cycle lives listed in the Requirement document. This requirement follows advice of an uncontained turbine blade release event which resulted from failure of the subject sleeve.