Document ID: chunk:federal_register_of_legislation:F2006B06568:body:0
Version: federal_register_of_legislation:F2006B06568
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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/RB211/8 H.P. Compressor Rotor Stage 4 to 6
                     Shaft Assembly - Life Limitation

 5/83

            CANCELLED.

            Background: Extensive laboratory investigation and stress analysis has now shown that the life restriction placed upon the affected assemblies by Rolls Royce RB211 SB211-72- 6420 can be removed. They can now assume the same life as their unaffected equivalent parts.