AD/RB211/17 - Intermediate Pressure Compressor Stage 6-7 Rotor Shafts

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

Legislation au F2006B06547 In force Legislative Instrument

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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/RB211/17 Intermediate Pressure Compressor

Stage 6-7 Rotor Shafts


10/95

 

Requirement: CANCELLED.

 

Background: The requirements of this Directive are now reflected in the Rolls Royce RB211 Time Limits Manual, chapter 5-10-01 and CAO 106, AD/ENG/7 refers.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.