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FAA AD on Pratt & Whitney Canada PW-206A and PW-206E turboshaft engines

Usa - To prevent turbine blade axial shift, which could cause high levels of vibration, loss of engine torque, in-flight engine shutdown, and loss of the airframe exhaust duct

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: August 20, 2004 (Volume 69, Number 161)] [Page 51547-51549] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NE-25-AD; Amendment 39-13775; AD 2004-17-03] RIN 2120-AA64 Airworthiness...

fra/pec - 102050

AVIONEWS - World Aeronautical Press Agency
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