S-10 Sakota

Climb ratio: 900 ft/min | 5 m/s
Glide ratio: 7:1

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

MEW (manufacturers empty weight): 231 kg | 510 lbs
MTOW (maximum takeoff weight): 458 kg | 1010 lbs

Engine: ROTAX 582, 912, 912 S or 914

Rans S10 Sakota

ROTAX 582 65 HP liquid cooled with dual CDI ignition; RPM gauge; 2-Blade wood prop; 4130 Welded steel fuselage, tail group and tapered steel landing gear; Aluminum wheels with aircraft tires; Wheel pants; Pre-formed trussed wing ribs; .020 Aluminum leading edge wrap; 3" Tubular Aluminum Main spars; 2" Tubular Aluminum Aft spars; (2) 9 Gallon wing tanks; Seat adjustable in tilt and fore and aft; 2.7 ounce aircraft covering fabric, all tapes, glue, and inspection plates; Aluminum framed canopy; Airfoil struts; In-flight pitch trim; In-flight start; "Deep Set" panel; Roll over protection; Shoulder harnesses and lap belts; Dual elevator horns; 1 1/4" Push-pull elevator tube; Cable operated rudder; 3-Position flaps; Differential ailerons are cable and push-pull tube operated; Dual control sticks and throttles; Center flap lever; Pre-molded cowling; 12" Composite spinner; Heavy duty engine mount; Under the wing windows; Dual fuselage foot pegs and wing steps; Dual wire braced folding tail; Steerable tail wheel; Dual rudder pedals; Hydraulic brakes; Firewall sound proofing; Baggage compartment.

The S-10 Sakota is an FAA Approved 51% Kit - No welding required.

The Rans S-10 Sakota build Time: 350 to 600 hours

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