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FAA AD on Taylorcraft, Inc. models A, B, and F series airplanes (2008-09-18)

Washington, Usa - To detect and correct corrosion or cracks in the wing strut attach fittings, which could result in failure of the wing strut attach fittings and lead to wing separation and loss of control

Airworthiness Directive Federal Register Information [Federal Register: May 2, 2008 (Volume 73, Number 86)] [Page 24162-24164] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0177; Directorate Identifier 2007-CE-093-AD; Amendment 39-15499; AD 2008-09-18] RIN 2120-AA64 Airworthiness Directives; Taylorcraft,...

fra/pec - 1089076

AVIONEWS - World Aeronautical Press Agency
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