STC - Data
- Type of Aircraft: F 406
- EASA STC: 10075453 (issued Feb 16, 2021)
- FAA STC: --
- Applicable Aircraft: ASI F406
- Engines: Pratt & Whitney PT6A-112
- Propeller: MTV-27-1-E-C-F-R(P)/CFR220-55( )
- Advantages:
- Best vibration damping characteristics for almost vibration free propeller operation
- Bonded on wide chord nickel alloy leading edges for superior erosion protection of the blades
- Smaller diameter of up to 16 cm (6 inch) compared to the original propeller, this means more ground
clearance
of about 8 cm (3 inch) for less FOD and also more clearance to the fuselage, therefore less cabin noise
from the prop tips
- Take-Off improvement up to 8%, so compared to the original AFM a higher safety for the calculated takeoff
run
- No propeller ADs
- TBO 4500 hours or 6 years, whatever comes first, for low maintenance costs
- No rpm restriction for the complete operational range
- The long-time proven MT-Propeller natural composite blades provide significant inside and outside noise
reduction
- No life limitation and repairable in case of an FOD
- Comply with the strict German noise regulations 2010 - „Landeplatz Lärmschutz Verordnung“ for
unrestricted airport operations in Germany and other European Countries
more
information about the STC (.pdf 106k)
MT-Propeller