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FAA (Correction) AD on Hamilton Sundstrand model 14RF-9 propellers

Washington, Usa - To prevent blade failure that could result in separation of a propeller blade and loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 19, 2006 (Volume 71, Number 97)] [Page 29072] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24517; Directorate Identifier 2006-NE-18-AD; Amendment 39-14591; AD 2006-10-07] RIN 2120-AA64 Airworthiness Directives; Hamilton...

fra/pec - 141362
Rome, Italy, 05/23/2006 11:54
AVIONEWS - World Aeronautical Press Agency

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