STC - Data
- Type of Aircraft: PA-60-600, -601, -601P, -602P, PA-60-700P
- EASA: 10062000 (issued July 18, 2017)
- FAA: SA04452NY (issued Nov. 2, 2021)
- Applicable Aircraft: PA-60-600, -601, -601P, -602P: modified according
to FAA STC SA1658NM
PA-60-700P
- Engines: Lycoming
IO-540-A- and IO-540-S-series. modified according
to FAA STC SE1657NM
(L)TIO-540-U-series
- 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)