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FAA AD on Bombardier model DHC-8-102, -103, and -106 airplanes
Washington, Usa - To prevent increased roll forces due to cracking of the left and right aileron tab actuator arm channels, which could be interpreted by the pilot as a flight control problem and might lead to loss of control of the airplane
Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41928-41930] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-339-AD; Amendment 39-13727; AD 2004-14-18] RIN 2120-AA64 Airworthiness...
fra/pec - 100454
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency