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FAA AD on Bombardier, Inc. model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes (2014-03-17)

Washington, Usa - To detect and correct incorrectly oriented or fractured fasteners, which could result in detachment of the flap hinge-box and the flap surface, and consequent reduced controllability of the airplane

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9389-9392] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2014-02977] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2014-0054; Directorate Identifier 2014-NM-001-AD; Amendment 39-17754; AD 2014-03-17] RIN...

fra/pec - 1158516

AVIONEWS - World Aeronautical Press Agency
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