STC - Data
- Type of Aircraft: PA-42-1000
- EASA: EASA:A.S.02480 (issued Dec 20, 2006)
- FAA: SA03487AT (issued Sept. 10, 2007)
- ANAC Brazil: 2016S10-16 (issued Oct. 20, 2016)
- INAC Venezuela: Letter of Acceptance to the
FAA STC SA03487AT
- TCCA Canada: SA23-97 (issued Dec. 4, 2023)
- 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)
MT-Propeller
