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FAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes (2005-11-10)

Washington, Usa - To prevent the loss of hydraulic power from both hydraulic systems, which could lead to reduced controllability of the airplane, and to prevent brake failure, which could result in the loss of directional control on the ground and

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32986-32988] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20756; Directorate Identifier 2004-NM-52-AD; Amendment 39-14112; AD 2005-11-10] RIN 2120-AA64 Airworthiness Directives; Bombardier...

fra/pec - 121748
Rome, Italy, 06/08/2005 11:53
AVIONEWS - World Aeronautical Press Agency

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