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FAA AD on Hamilton Sundstrand Propellers model 568F propellers (2009-07-06)

Washington, Usa - To prevent cracks from developing in the tulip area of the blade, which could result in separation of the blade and loss of airplane control

Airworthiness Directive Federal Register Information Federal Register: [Page 13337-13339] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0270; Directorate Identifier 2008-NE-30-AD; Amendment 39-15865; AD 2009-07-06] RIN 2120-AA64 Airworthiness Directives; Hamilton Sundstrand Propellers Model 568F Propellers...

fra/pec - 1102866

AVIONEWS - World Aeronautical Press Agency
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