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FAA AD on Bombardier model DHC-8-100, DHC-8-200, DHC-8-300, and DHC-8-400 series airplanes
Washington, Usa - To prevent shear failure of control column torque tube rivets, which could cause unexpected decoupling of the elevators and large unwanted deflection of the free elevator, and consequent reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: August 25, 2006 (Volume 71, Number 165)] [Page 50331-50333] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24979; Directorate Identifier 2006-NM-014-AD; Amendment 39-14738; AD 2006-17-17] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 147810
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency