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| S-19 | |||
Specifications and Performance |
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| SPECIFICATIONS | |
| Wing Span | 28 ft |
| Area | 126.9 sq ft |
| Mean Chord | 4 ft 7 in |
| Aspect | 6.18 |
| Height | 95.5 in |
| Cockpit Width | 43.5 in |
| Number of Seats | 2 |
| Landing Gear* | F/TR |
| Baggage Volume | N/A |
| Baggage Capacity | 70 lbs |
| Fuel Capacity | 24 gal US |
| POWER PLANT | 912S |
| Engine | Rotax 912S |
| Output | 100 HP |
| Oil Capacity | 3.0 qts |
| Coolant Capacity | 4.4 qts |
| Propeller Diameter | 68 in |
| Propeller Type | 2 Blade ground adjustable |
| Gear Reduction | 1:2.43 |
| Fuel G.P.H. | 5.0 gal @ 75% |
| PERFORMANCE | |
| Take Off Roll | 325 ft |
| Rate of Climb | 900 fpm |
| Service Ceiling | 14,500 ft |
| Cruise | 128 mph |
| VNE | 150 mph |
| Stall Clean | 51 mph |
| Stall Flaps | 45 mph |
| Landing Roll | 325 ft |
| CRUISE PERFORMANCE @ 7500 ft Max Weight | |
| Cruise (@75%) | 128 mph |
| Fuel Consumption (75%) | 5.0 gal/hr |
| Endurance (@75%) | 4.55 hrs |
| Range (@75%) | 580 miles |
| Cruise (@65%) | 120 mph |
| Fuel Consumption (@65%) | 4.5 gal/hr |
| Endurance (@65%) | 5.10 hrs |
| Range (@65%) | 610 miles |
| WEIGHTS AND LOADINGS | |
| Gross Weight | 1320 lbs |
| Empty Weight | 820 lbs |
| Useful Load | 500 lbs |
| Wing Loading | 10.4 psf |
| Power Loading | 13.2 lb/HP |
| Limit Load Factors | +4.4 -2 |
| *F/TR = Fixed /Trike | |
| Performance at sea level and maximum gross weight except otherwise stated. | |
| Standard Equipment and Features | |
| ROTAX engine install kits available; Wing spar factory assembled with solid rivets and ready for installation; Airframe is of all aircraft grade aluminum construction; Pull type rivets used throughout entire airframe (except for wing spar); All parts are produced on CNC machines for highest level of precision and quality; Forming of all parts is completed (only minor forming requiring no special tools is left to builder); Wings and fuselage can be built without special fixtures; Vertical fin, stabilizer and rudder fixtures are provided; All hardware; Molded tips for wing, stabilizer and vertical fin; Removable inspection plates throughout the airframe; 5" nose and main gear wheels and tires; 2 piece spring aluminum main gear; steerable nose gear, dual rudder pedals, hydraulic brakes (pilot side std); Upholstered seats; Dual control sticks; Elevator trim system; Wings detach for storage; Stabilizer detaches for storage; 12 gallon plastic molded wing tank (each wing); Fuel valve, electrical backup pump, all fittings, drains, vent tubes and lines for fuel system; Pitot static system with wing mounted probe; Tie down fittings for wings and tail; Lap and shoulder belts ( 4 point); Stabilator operated via push pull tubes; Differential Ailerons operated via push pull tubes; Rudder operated via 1/8" aircraft grade cable on pulleys; Adjustable stops on all controls; Baggage floor; Bulkhead close-out (forms baggage area) | |
| Engine Install Kit | |
Includes everything needed to install the Rotax 912S minus the engine itself, a very complete and detailed kit including carburetor heat, cabin heat, exhaust, cooling system, filters and miscellaneous, parts. Standard instruments with 912S Engine Install kit: RPM, Hour Meter, CHT, Voltage meter, Oil Temperature, and Oil Pressure gauge. Build Time: 700 to 1000 hours |
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