MT PA42-1000
STC – Data
Type of Aircraft: PA-42-1000
EASA: EASA:A.S.02480 (issued Dec 20, 2006)
FAA:
(issued Sept. 10, 2007)
Applicable Aircraft: Piper PA-42-1000 (Cheyenne 400LS)
Engines: Honeywell TPE331-14A/B
Propeller: MTV-27-1-E-C-F-R(G)/CFR(L)250-103
Advantages:
- Best vibration damping characteristics
- Bonded on nickel alloy leading edge for best erosion
protection of the blades - Take-off distance over 50 ft obstacle
reduced by approx. 5% (SL, ISA, MTOW) - Enhanced climb by approx.3% (SL, ISA conditions, MTOW)
increasing by altitude - Enhanced cruising speeds by approx. 5 kts +
(ISA, FL250, 11500 lbs GW) - Approx. 52 lbs less total weight than the orig. propellers
- Significant inside and outside noise reductionsS
- Unlimited blade life
- FOD repairable blades
more information about the STC (.pdf 65k)
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