E-LSA possible – KIS TR1 2 seater located in NC $37,500 with 0-235 engine $27,000 without engine

Kis TR1

30 Year Proven Track Record

Simple 2 Place Airplane

Efficient All Composite like 2 Place Cirrus

Affordable Kit Plane

135 ktas @ 6.3 gph @ 8′ ft @ 75% 0-235 Lycoming 115 HP Engine

160 ktas @ 7 gph @ 8′ ft @ 75% Aerovolare 160 HP Turbo Engine

PRICE

$27,000 – not fully completed without engine

$37,500 – not fully completed with 0-235 engine

$97,000 – complete flying with 0-235 engine or other similar engine and Dynon Avionics. Available in 6-12 months.

Achieving 160 ktas super-fast speeds is possible with AV 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 @ 8 gph.

Located in Whiteville, NC.

SPECS

Max take off gross weight: 1450 lbs

Empty weight: 850 lbs

Useful Load: 600 lbs

Range: 660 NM

Fuel Capacity: 33 gallons

E-LSA – 1320 lbs with 470 lbs useful load

PERFORMANCE

Stall speed: 40 kts IAS
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 – 1082 ft
E-LSA Take off – 962 ft (lower max weight)
Take-off distances: 1312 ft / 2132 ft to clear 50 ft (at MTOW and sea level)
Landing distances: 1300 ft (at MTOW and sea level)
Fuel consumption: 6,3 gal/hour per flight time at 75% cruise. (O-235)
8 GPH 75% cruise with Aerovolare 160 HP turbo – 160 ktas @ 8,000 ft

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 O-235
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 10

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

FLAPS
Flap Type Plain
Area/Wing 12 %
Length (Each) 65 in.
Chord 12.5 in. = 28% c

CONTROL MOVEMENT
Elevator +25 – 16 degrees
Ailerons +12 – 12 degrees
Rudder L 25 R 30 degrees
Flaps 0/12/28

LIMITATIONS
Limit Load Factor +4.4 G
Design Limit Load Factor -2.2 G
V-Maneuver Speed 113 kts
V-f Flap Ext. Speed 96 kts
V-ne Never Exceed Speed 188 kts

MAIN LANDING GEAR
Type One Piece Alloy Alum.
Wheels Matco 6 x 6
Tires McCreary 6 x 6 (13.5 in.dia.)
Brakes Toe Actuated Disk/Caliper Hyd.Piston

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%

PLACARDED IAS LIMITS
Green Arc 40 to 136 kts
Yellow Arc 136 to 188 kts
White Arc 40 to 96 kts
Red Line 188 kts

NOSE LANDING GEAR
Type Fabricated Steel Free Swiveling
Wheel Matco 5 x 5 Alloy Alum.
Tire Lamb 5 x 5 (11.5 in. dia.)

Total weight of 180kg (400 lbs).

Maximum allowable baggage weight is 27 kg (60lbs).