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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

Washington, Usa - To prevent engine fuel starvation during maximum climb and descent caused by poor fuel tank venting with low fuel levels, which could result in a loss of engine power during critical phases of flight

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35783-35785] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24091; Directorate Identifier 2006-CE-17-AD; Amendment 39-14665; AD 2006-13-12] RIN 2120-AA64 Airworthiness Directives; Pilatus...

fra/pec - 143386

AVIONEWS - World Aeronautical Press Agency
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