AD/RRT-S/10 - HP2 Turbine Disc Locating Sleeve

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06679 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.