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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: December 13, 2005 (Volume 70, Number 238)] [Page 73576-73577] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NE-38-AD; Amendment 39-14404; AD 2005-25-11] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce plc RB211 Trent 800 Series...

fra/pec - 132934
Rome, Italy, 12/14/2005 14:05
AVIONEWS - World Aeronautical Press Agency

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