Document ID: chunk:federal_register_of_legislation:F2006B06545:body:0
Version: federal_register_of_legislation:F2006B06545
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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/RB211/15 IP Compressor Stage 6-7 Rotor Shaft Life 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.