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Performance Information
Development Schedule
Ordering Information

Performance Information*:

The Transition® is being designed to be a factory certified Light-Sport Airplane.
Two seats, side-by-side.
GTOW: 1320 lbs (600 kg)
Fuel: Super-unleaded autogas
Fuel Capacity: 20 gal (120 lbs / 54 kg)
Fuel Consumption (75% power): 4.5 gph
Engine: 100 hp Rotax 912 S (four-stroke)
Vs = 45 kts (51 mph, 83 km/hr)
Vr = 70 kts (80 mph, 130 km/hr)
Cruise Speed: 100 kts (115 mph, 185 km/hr)
Range: 400 nm (460 mi, 740 km)
Takeoff Distance over 50 ft obstacle: 1,700 ft (520 m)
Wingspan: 27.5 ft (8.4 m)
Length: 18.75 ft (5.7 m)
Height: 6.75 ft (2.1 m)
On-Road Width: 6.5 ft (2.0 m)
Capable of highway speeds on the road.

Development Schedule*:

Proof of Concept drive and flight testing, Fall-Winter 2008.
First delivery: late 2009
Production schedules are filling up -- act now!

* All information contained here is preliminary and subject to change without notice.