XT2000
XT2000 Specifications
(Experimental Homebuilt, Kit only)
Included equipment
Electric start
Day VFR panel
Engine monitor
Nose wheel steering
Main wheel brakes
Optional
Altitude compensating Fuel injection
Aircraft
Wing Span 30’
Wing chord 5′
Wing area 150 sq. ft.
Wing surface 35% double
Wing type 3 strut ladder
Wing style rectangular
Empty weight 350#
Gross weight 1000’ max
Wing loading 6.7 lbs./sq. ft. at gross
Load factor +6 –3 G
Length 16’
Height 9′
Seating 2
Fuel capacity 10-20 gallons
Standard engine and drive
Engine make Hirth 3203E
Engine type twin cylinder inline
Engine style 2 stroke
Cooling Forced air fan
Mounting inverted pusher
Starter electric
Oil system injection
Horsepower 65 hp/6500 rpm
Torque 55 ft. lb./6000 rpm
Ignition dual CDI
Timing electronic module
Spark plugs 4
Carburetors 2
TBO 1000 hrs / 75% power
Reduction gear
Drive ratio 2.59 to 1
Rotation clockwise
Performance (depends on weight)
Top speed 70+ knots
Cruise speed any
Max speed 80 knots (tested not Vne)
Stall speed 20-25 knots
Take off roll 100-125’
Landing roll 125-150′
Sea level climb >1200’/minute
Range 300 miles (depends on fuel)
Ceiling (tested) 15,000’
Specifications are subject to change at any time
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