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FAA AD on Bombardier model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) series airplanes
Washington, Usa - To detect and correct gaps between the flap vane bracket and the adjacent lower skin and between the flap vane bracket and vane actuator beam of the wing flap systems, and premature cracking of the flap vane brackets, which could result
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-317-AD; Amendment 39-13125; AD 2003-08-12] RIN 2120-AA64 Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Series Airplanes PDF Copy (If Available): Preamble...
AVIONEWS - World Aeronautical Press Agency - 44482
AVIONEWS - World Aeronautical Press Agency
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AVIONEWS - World Aeronautical Press Agency