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FAA AD on Honeywell International Inc. TFE731-2C, -3B, -3BR, -3C, -3CR, -3D, -3DR, -4R, -5AR, -5BR, -5R, -20R, -20AR, - 20BR, -40, -40AR, -40R, and -60 series turbofan engines (2008-02-19)

Washington, Usa - To prevent uncontained failure of the HP turbine rotor assembly, which could result in damage to the airplane

Airworthiness Directive Federal Register Information Federal Register: January 31, 2008 [Page 5735-5737] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27891; Directorate Identifier 2007-NE-14-AD; Amendment 39-15349; AD 2008-02-19] RIN 2120-AA64 Airworthiness Directives; Honeywell International Inc. TFE731-2C,...

fra/pec - 1085395

AVIONEWS - World Aeronautical Press Agency
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