Rans S-10 Sakota

by Rans Designs Inc.
3.5
6
Rans S-10 Sakota - Photo #1

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

 

Specifications

Empty weight:
510 lbs (231 kg)
MTOW:
1010 lbs (458 kg)
Stall speed:
42 kts (48 mph) (78 kph)
Cruise speed:
104 kts (120 mph) (193 kph)
VNE:
113 kts (130 mph) (209 kph)
Climb:
900 ft/min (4.6 m/s)
Glide ratio:
7
Take-off distance:
500 ft (152 m)
Landing distance:
500 ft (152 m)
Engine:
Rotax 582, 912, 912 S or 914

PHOTOS

Rans S-10 Sakota - Photo #2
Rans S-10 Sakota - Photo #3

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