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AD/RB211/15 - IP Compressor Stage 6-7 Rotor Shaft Life
1AD/RB211/15 - IP Compressor Stage 6-7 Rotor Shaft Life
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.