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FAA AD on Dornier model 328-100 and -300 series airplanes (2004-09-16)
Usa - To prevent failure of the rudder flight control system due to cracking of the bearing lugs of the rudder spring tab lever assembly, which could result in loss of rudder control 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 24953-24954] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-263-AD; Amendment 39-13605; AD 2004-09-16] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 63010
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency