STC - Data
- Type of Aircraft: CA185E, -F
- LBA: SA1391 (issued July 26, 2004)
- FAA: SA 01296WI (issued Dec. 06, 2004)
- TCCA: Letter of Acceptance of EASA STC (issued Dec. 16, 2019)
- INAC Venzuela: Letter of Acceptance to the
FAA STC SA01296WI (issued Aug 16, 2017)
- Applicable Aircraft: Cessna A185E, -F
- Engines: TCM IO-520-D
- Propeller: MTV-15-D/210-58
- Advantages:
- Best vibration damping characteristics
- Bonded on stainless steel leading edge for best erosion
protection of the blades
- Shorter take-off distance by approx. –10 %
(SL, ISA conditions)
- Enhanced climb by approx. 5% (SL, ISA conditions)
- Cruise performance increased by 3 to 5 kts
(MTOW, ISA conditions)
- Approx. 10 lbs to 30 lbs less weight than the original propeller
- Significant inside and outside noise reductions
- Unlimited blade life
- FOD repairable blades
more
information about the STC (.pdf 80k)