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FAA AD on Eurocopter France model EC-155B, EC-155B1, SA-365N, SA-365N1, AS-365N2, and AS-365N3 helicopters

Washington, Usa - To prevent failure of a hose, resulting in failure of hydraulic pressure to the brakes on the affected landing gear wheel, and subsequent loss of control of the helicopter during a run-on landing

Airworthiness Directive Federal Register Information [Federal Register: June 24, 2005 (Volume 70, Number 121)] [Page 36482-36484] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20512; Directorate Identifier 2004-SW-35-AD; Amendment 39-14160; AD 2005-13-23] RIN 2120-AA64 Airworthiness Directives; Eurocopter...

fra/pec - 122819
Rome, Italy, 06/27/2005 13:58
AVIONEWS - World Aeronautical Press Agency

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