Aircraft

Veloce Planes
Phone: 773-620-9500

Contact Veloce Planes

Aircraft Summary
  • Kis TR1 - EAB or E-LSA Possible - 30 Year Proven Track Record
  • Simple 2 Place Airplane Efficient All Composite like 2 Place Cirrus Affordable Kit Plane

  • Immediate delivery:
  • $19,700 - 90% completed kit without engine.
  • $29,700 - 90% completed kit with 0-235 engine or other similar engine.

  • Available in 6-9 months:
  • $77,000 - complete flying with 0-235 engine, AV 160 HP Turbo engine, or similar, and Dynon Avionics.
  • $97,000 - complete flying with 141 HP Rotax 915.

  • http://www.VelocePlanes.com/tr1

  • AV 160 HP
  • - Achieving super-fast speeds is possible with our 160 HP Turbo Engine.
  • - We've redesigned the rudder and tail for this specific a 160 HP Turbo Engine, offering it to you for $15k.
  • - This engine is a Suzuki based 1500 cc engine with turbo and air trike redrive.
  • - It has a track record of over 2000 flying hours across 20 years without incidents.
  • - These engines are bullet proof from anyone who knows.
  • - It's been used in boats at 5,000 RPMs for 5,000 hours regularly.
  • - It has covered 500,000 miles in vehicles.
  • - With this engine, the plane can reach speeds of 160 ktas @ 7 gph.

  • SPECS

  • Max take off gross weight: 1450 lbs
  • Empty weight: 850 lbs
  • Useful Load: 600 lbs

  • PERFORMANCE
  • Stall speed: 40 kts IAS (50 kts CAS)
  • Climb angle: 6.2 deg @70 kts and MTOW
  • Rate of climb: 850 (heavy) 1200 (light) fpm @ 80 kts at sea level
  • Max speed in turbulent air: 136 kts
  • Glide data: best speed 80 kts IAS. 2 NM per 1000'.
  • Approach speeds: 70-75 kts clean, 65-70 kts w/flap.
  • Take-off distances: 400 m / 650 m to clear 15 m (at MTOW and sea level)
  • Landing distances: 400 m (at MTOW and sea level)
  • Fuel consumption: 24 liter/hour per flight time at 75% cruise.

  • AIRSPEED LIMITATIONS
  • Never exceed (Vne): 188 kts (216 mph)
  • Vno: 136 kts (156 mph)
  • Maximum Flap Speed (Vfe): 96 kts (110 mph)
  • Maneuvering speed (Va): 113 kts (130mph)
  • Stall speed - no flap: 40 kts IAS (50 kts CAS)
  • Stall speed - flap: 40 kts IAS (50 kts CAS)

  • ENGINE OPERATION LIMITATIONS
  • Crankshaft Speed - RPM
  • Rated Maximum continuous Operation 125 HP @ 2800
  • Recommended Max. For Cruising. 94 HP @ 2550
  • Recommended Min for Idle 700+25
  • Maximum Take-off Full Throttle
  • Maximum Continuous. Full Throttle
  • Fuel Grade: 100LL or 100

  • Total weight of 180kg (400 lbs).
  • Maximum allowable baggage weight is 27 kg (60lbs).


    Engines:
  • O-235
Remarks
  • DIMENSIONS OVERALL
  • Length 22 ft.
  • Wing Span 23 ft.
  • Height (Top of tail) 7.25 ft.
  • Height (Top of cockpit) 5.65 ft.
  • WING DIMENSIONS
  • Wing Area 88 sq.ft.
  • Chord 3.83 ft.
  • Aspect Ratio 6
  • Spar Location 30% of Chord
  • Airfoil NACA 63(2)-215
  • Dihedral (per panel) 2.5 degrees
  • Tip Wash Out 0 degrees
  • Wing Loading 16.5
  • FUSELAGE DIMENSIONS
  • Frontal Area 9.0 sq. ft.
  • Cockpit Width 42 in.
  • Cockpit Height 39 in.
  • Cockpit Length 65 in.
  • TAIL DIMENSIONS
  • Horizontal Tail Span 7.33 ft.
  • Horz. Tail Chord 2.08 ft.
  • Horz. Stab. Mean Chord 1.33 ft.
  • Elevator Mean Chord .75 ft.
  • Horz. Tail Area 15.2 sq.ft.
  • Horz. Tail Aspect Ratio 3.5
  • Horz. Tail Thickness 12 %
  • Vertical Tail Height 4.09 ft.
  • Vertical Tail Mean Chord .83 ft.
  • Dorsal Fin .33 x 2.5 ft.
  • Vertical Fin Thickness 10%