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FAA AD on Pilatus Aircraft Ltd. models PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes (2006-15-02)

Washington, Usa - To detect and correct increased friction in the aileron control bellcrank assemblies, which could result in failure of the aileron flight-control system

Airworthiness Directive Federal Register Information [Federal Register: July 19, 2006 (Volume 71, Number 138)] [Page 40888-40891] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24092; Directorate Identifier 2006-CE-18-AD; Amendment 39-14682; AD 2006-15-02] RIN 2120-AA64 Airworthiness Directives; Pilatus...

fra/pec - 145447

AVIONEWS - World Aeronautical Press Agency
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