Aircraft Model(s): Piper PA-46-500TP
Applicable Engines: PT6A-42A engine
|1||5-Bladed ASCII Composite Propeller||5D3-N338A1/78D01B|
|1||STC Document Set||SA04045CH|
|1||Airframe De-ice Kit||106337|
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)
Hartzell – 82.5” HC-E4N-3Q/E8501B-3.5 4-bladed aluminum
4000 hours/6 year TBO
Diameter: to 82.5” Max., 81.5” min.
MT-Propeller 79.92” 5 blade MTV-27-1-E-C-F-R(P)/CFR203-58d
with laminated wood blades
3000 hours/6 years
142 lb (prop w/de-ice)
Carbon fiber construction allowing for thinner, stiffer airfoil
design for better all around performance.
20% greater take-off acceleration.
90 fpm better ROC at Vy.
2-3 knots cruise speed increase.
Significantly reduced weight.
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. 1.9 dB(a) reduction from standard airplane.
No change in RPM limitations or placards.
Strongest material available with field replaceable nickel steel
leading edge erosion shield – no lost performance
due to reduced diameter.
Best Warranty in the industry along with worldwide support.
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