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VS (stall speed): 36 kts | 41 mph | 66 kph
VC (cruise speed): 78 kts | 90 mph | 145 kph
VNE (never exceed speed) : 104 kts | 120 mph | 193 kph
Climb ratio: 1100 ft/min | 6 m/s

Takeoff distance over 50ft (15m) obstacle: 200 ft | 61 m
Landing distance over 50ft (15m) obstacle: 500 ft | 152 m

MEW (manufacturers empty weight): 249 kg | 550 lbs
MTOW (maximum takeoff weight): 454 kg | 1000 lbs

Engine: Rotax 582, 912
Fuel consumption: 4.1 gph

In 1990, after the FAA allowed for heavier 2-place ultralights, the same basic TwinStar Mark II design was strengthened (main spars increased from 5” to 6” diameter) to carry the more powerful Rotax 582 engine and also to increase the gross weight to 1000 lb. resulting in the TwinStar Mark III.

In 1993, the Mark III lite was introduced. The lite version was discontinued in 1994 as most people wanted the flaps which the Lite version did not have.

Cabin width is 42 inches and entrance is through one of the two gull wing style doors.


Price: 18700 USD

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Empty weight: 295 kg | 650 lbs

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