Piper PA34-() Seneca II, III, IV, V
- Piper PA-34 with 3-blade MTV-12
STC - Data
- Type of Aircraft: PA-34 Seneca II- V
- EASA: EASA.A.S.02553 (issued March 13, 2006)
- FAA: SA03434AT (issued April 19, 2007)
- Applicable Aircraft: PA-34-200T, PA-34-220T
- Engines: TCM TSIO-360-E, -EB, -KB, -RB
- Propeller: MTV-12-D-C-F/CFL188-53 (right wing)
MTV-12-D-C-F/CF188-53 (left wing)
- Best vibration damping characteristics
- Bonded on stainless steel leading edge for best erosion
protection of the blades - Enhanced Climb by approx. 5% (MTOW, ISA conditions)
- Cruise performance increased by approx. 3 to 5 kts
(MTOW, ISA conditions) - Approx. 10 lbs less weight than the original
3-blade propellers - Significant inside and outside noise reductions
- Increased ground clearance for less blade tip erosion
- Unlimited blade life
- FOD repairable blades
more information about the STC (.pdf 80k)
