2023 VELOCE PLANES VELOCE 200


  • For Sale
  • 2023
  • VELOCE PLANES VELOCE 200
  • Not Listed
  • Not Listed
  • Whiteville, NC USA

97000 $97,000 USD
$37.500 not completed w/ o-235

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  • For Sale
  • 2023
  • VELOCE PLANES VELOCE 200
  • Not Listed
  • Not Listed
  • Whiteville, NC USA

General Specs (cont.)

0

Used

2023

2023

2

Additional Classifications

Detailed Description

E-LSA Possible

Kis TR1 
30 Year Proven Track Record
Simple 2 Place Airplane
Efficient All Composite like 2 Place Cirrus
Affordable Kit Plane

Complete flying for $97k with o-235 engine or other similar engine and Dynon Avionics.
Available in 6-12 months. 

- 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.

Price
$97,000 completed with o-235 engine or other similar engine and Dynon Avionics. Available in 6-12 months.
$37,500 not completed with 0-235 engine or other similar engine.
$27,000 not completed without engine.

http://www.VelocePlanes.com/tr1

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 / Mods / Prop

0-235

Interior / Exterior

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%