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FAA AD on Rolls-Royce plc RB211-524 series turbofan engines

Washington, Usa - To prevent IP (Intermediate pressure) compressor stage 5 disk failure, which could result in uncontained engine failure and possible damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 26, 2005 (Volume 70, Number 142)] [Page 43036-43039] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-40-AD; Amendment 39-14202; AD 2005-15-13] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan...

fra/pec - 124441
Rome, Italy, 07/27/2005 14:19
AVIONEWS - World Aeronautical Press Agency

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