STC - Data
- Type of Aircraft: PA-60-600, -601, -601P, -602P, PA-60-700P
- EASA: 10062000 (issued July 18, 2017)
- FAA: i.p.
- Applicable Aircraft: PA-60-600, -601, -601P, -602P, PA-60-700P
- Engines: Lycoming
IO-540-S1A5-MM, IO-540-AA1A5-MM,
(L)TIO-540-U2A
- Propeller: MTV-14-B-C-F/CF(L)188-30g
- Advantages:
- Best vibration damping characteristics
- Bonded on stainless steel leading edge for best erosion
protection of the blades
- Shorter take-off distance
- Enhanced climb by approx. 3% to 5% (SL, ISA conditions)
- Cruise performance increased by approx. 3 to 5 kts
(MTOW, ISA conditions)
- Approx. 40 lbs less weight than the original propellers
- Unlimited blade life
- No airframe resonance with low engine rpm
- Significant inside and outside noise reductions
more
information about the STC (.pdf 190k)