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FAA AD on Rolls-Royce plc RB211 Trent 800 series turbofan engines

Washington, Usa - To prevent possible multiple uncontained LP compressor fan blade failure, due to cracking in the blade root caused by increased stresses in the shear key slots

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 28, 2004 (Volume 69, Number 144)] [Page 44925-44927] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NE-38-AD; Amendment 39-13736; AD 2004-15-02] RIN 2120-AA64 Airworthiness...

fra/pec - 100847
Rome, Italy, 07/29/2004 12:32
AVIONEWS - World Aeronautical Press Agency

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