XT1000
XT1000 Specifications
(Experimental Homebuilt, kit only)
Included equipment
Electric start
Day VFR panel
Engine monitor
Nose wheel steering
Nose wheel brake
Optional
Altitude compensating Fuel injection
Main gear brakes
Other engine choices (custom order)
Aircraft
Wing Span 30′
Wing Chord 5′
Wing area 150 sq. ft.
Wing surface 35% double
Wing type 3 strut ladder
Wing style rectangualar
Empty weight 300+#
Gross weight 750’ max
Wing loading 5.0 lbs./sq. ft. at gross
Load factor +6 –3 G
Length 15’
Height 9′
Seating 1
Fuel capacity 10-15 gallons
Standard engine and drive
Engine make Hirth F23LW
Engine type twin cylinder opposed
Engine style 2 stroke
Cooling free air
Mounting inverted pusher
Starter electric
Oil system injection
Horsepower 50 hp/6200 rpm
Torque 45 ft. lb./6150 rpm
Ignition dual CDI
Timing electronic module
Spark plugs 4
Carguretors 2
TBO 1000 hrs / 75% power
Reduction multi V belt
Belt life 500 hrs
Drive ratio 2.5 to 1
Rotation counter clockwise
Thrust 300’
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 75’
Landing roll 100’
Sea level climb >1000’/minute
Range 300 miles (depends on fuel)
Ceiling (tested) 15,000’
Specifications are subject to change at any time
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