Rans S-10 Sakota taildragger

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Rans S-10 Sakota taildragger Specifications and Images

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Length: 17 ft 10 in (5.44 m)
Wingspan: 24 ft 0 in (7.32 m)
Height: 4 ft 10 in (1.47 m)
Wing area: 95 sq ft (8.8 m2)
Aspect ratio: 4.23:1
Empty weight: 460 lb (209 kg)
Gross weight: 960 lb (435 kg)
Fuel capacity: 18 US gallons (68 litres)
Powerplant: 1 × Rotax 582 , 64 hp (48 kW)
Propellers: 2-bladed wooden, 5 ft 10 in (1.78 m) diameter

Performance
Cruise speed: 110 mph (96 kn; 177 km/h)
Stall speed: 45 mph (39 kn; 72 km/h)
Never exceed speed: 130 mph (113 kn; 209 km/h)
Range: 341 mi (296 nmi; 549 km)
Endurance: 3.1 hrs
Service ceiling: 12,500 ft (3,810 m)
G limits: +4/-2 at max gross weight and +6/-4 at 670lbs.
Roll rate: 100 degrees/sec
Maximum glide ratio: 7:1
Rate of climb: 800 ft/min (4.1 m/s)
Wing loading: 10.1 lb/sq ft (49 kg/m2)


Rans S-10 Sakota Video

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Ultralight Aircraft Magazine - Welcome to the Ultralight Aircraft News our goal is to cover as many aircraft expositions that host aircraft described as ultralight aircraft, light sport aircraft, experimental light sport aircraft, amateur built aircraft, ELSA or homebuilt aircraft that fit into the definition of ultralight aircraft in Canada or light sport aircraft, or experimental amateurbuilt light sport aircraft in the United States. 

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