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FAA AD on Hamilton Sundstrand Corporation Model 568F-1 propellers
Washington, Usa - To prevent blade failure due to corrosion-induced fatigue
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-02-AD; Amendment 39-12831; AD 2002-15-03] RIN 2120-AA64 Airworthiness Directives; Hamilton Sundstrand Corporation Model 568F-1 Propellers. Preamble Information Regulatory Information 2002-15-03 Hamilton Sundstrand Corporation: Amendment...
AVIONEWS - World Aeronautical Press Agency