Aircraft Model(s): Piper PA-46-600TP
Applicable Engines: PT6A-42A
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Hartzell 82.5” inch diameter 5-bladed, all carbon Advanced Structural Composite, Second Generation (ASC-II), swept-tip, scimitar composite blades with all new lighter-weight aluminum “Raptor®” hub propeller.
4000 hour / 6 year TBO
128.8 pounds (prop and spinner)
Carbon fiber construction allowing for thinner, stiffer airfoil design for better all around performance
Measured take-off and climb noise number of 74.9 dB(a) complies with both FAR Part 36, Appendix G, and ICAO, Annex 16, Chapter 10 by a wide margin.
Strongest material available with field replaceable nickel steel leading edge erosion shield – no lost performance due to reduced diamater
Best warranty in the industry along with worldwide support
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