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FAA AD on Turbomeca Turmo IV A and IV C series turboshaft engines
Washington, Usa - To prevent centrifugal compressor intake wheel blade cracks, which can result in in-flight engine power loss or shutdown
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NE-12-AD; Amendment 39-13168; AD 2003-11-09] RIN 2120-AA64 Airworthiness Directives; Turbomeca Turmo IV A and IV C Series Turboshaft Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-11-09 Turbomeca: Amendment...
AVIONEWS - World Aeronautical Press Agency - 46112
AVIONEWS - World Aeronautical Press Agency
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AVIONEWS - World Aeronautical Press Agency