MT Piper PA-42/42-720
STC – Data
Type of Aircraft: PA-42/42-720
EASA: EASA.A.S.03604 (issued Oct 2008)
FAA: i.p.
Applicable Aircraft: Piper PA-42 Cheyenne III
Piper PA-42-720 Cheyenne IIIA
Engines: PT6A-41, PT6A-61
Propeller: MTV-16-1-E-C-F-R(P)/CFR230-37b
Advantages:
- Best vibration damping characteristics
- Bonded on stainless steel leading edge for best erosion
protection of the blades - Enhanced take-off distance and Climb Performance
(MTOW, ISA) - Cruise performance increased with 1800 RPM by
approx. 4 to 5 kts (Mid GW, ISA) - Approx. 60 lbs less weight than the original propellers
- More ground clearance for less FODs
- Significant inside and outside noise reductions
- Noise level is below 80 dB(A) according to
ICAO Annex 16 Chapter 10 - Cabin noise is reduced by 4 to 6 dB(A)
- Unlimited blade life
- FOD repairable blades
more information about the STC (.pdf 70k)
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