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FAA AD on Eurocopter France model AS-350B, BA, B1, B2, B3, C, D, D1, and EC-130B4 helicopters (2005-03-08)

Washington, Usa - To prevent a fuel bleed lever from separating and striking the tail rotor blade (blade), resulting in damage to or loss of a blade, and subsequent vibration and loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: February 14, 2005 (Volume 70, Number 29)] [Page 7381-7382] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19038; Directorate Identifier 2004-SW-24-AD; Amendment 39-13964; AD 2005-03-08] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 114293
Rome, Italy, 02/15/2005 14:46
AVIONEWS - World Aeronautical Press Agency

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