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FAA AD on Dornier model 328-100 and -300 series airplanes (2004-09-17)
Usa - To prevent fracture and/or breakage of the hinge bolt of the output rod of the rudder spring tab lever assembly, which could result in migration of the bolt tail, a loose spring tab, and consequent reduced controllability of the airplane
Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24952-24953] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-120-AD; Amendment 39-13606; AD 2004-09-17] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 63013
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency