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FAA AD on Pratt & Whitney Canada PT6A series turboprop engines
Washington, USA - To prevent failure of the turbine exhaust duct due to cracking that could result in possible separation of the reduction gearbox and propeller from the engine, and possible loss of control of the airplane
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NE-44-AD; Amendment 39-12957; AD 2002-23-13] RIN 2120-AA64 Airworthiness Directives; Pratt & Whitney Canada PT6A Series Turboprop Engines PDF Copy (If Available): Preamble Information Regulatory Information 2002-23-13 Pratt & Whitney...
AVIONEWS - World Aeronautical Press Agency - 36446
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency