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FAA AD on Gulfstream model G-1159, G-1159A, G-1159B, and G-IV series airplanes
Washington, Usa - To detect and correct broken damper shafts, which could result in locking of an aileron or elevator actuator (hard-over condition), subsequent loss of aileron or elevator control, and consequent reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: October 18, 2004 (Volume 69, Number 200)] [Page 61305-61309] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19337; Directorate Identifier 2004-NM-155-AD; Amendment 39-13824; AD 2004-21-03] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 105649
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency