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Airplane VL-3C – 1
The plane has been derived from basic VL-3 plane respecting American LSA rules. It has a larger, newly shaped wing and is produced with fixed landing gear and on land adjustable propeller. Strength test were carried out for MTOW 600 kg (1320 lbs).
Weights and Capacities
| Wingspan | 31'6'' |
| Height | 6'11'' |
| Fuselage Length | 20'4'' |
| Cabin Width | 42" |
| Prop Diameter | 5'8'' |
| Empty Weight | 760 lbs |
| Maximum Gross Weight | 1,320 lbs |
| Useable Fuel (US) | 29 gal |
| Useful Load | 560 lbs |
| Full Fuel Payload | 390 lbs |
Aircraft performance, capabilities and speeds
| Take-off Distance [ground roll] | 520 ft |
| Landing Distance [ground roll] | 550 ft |
| Take-off Distance [to clear a 50’ obstacle] | 1,050 ft |
| Landing Distance [to clear a 50’ obstacle] | 1,100 ft |
| Sea Level Climb Rate | 850 fpm |
| Service Ceiling | 13,200msl |
| Maximum Range | 730 nm |
| Fuel Flow | 3.8 gph |
| Maximum Cruise Speed | 119 ktas |
| Stall Speed [Vs0—Landing Configuration] | 35 kts |
| Stall Speed [Vs1—Clean] | 45 kts |
| Best Rate of Climb [Vy] | 65 kts |
| Maneuvering Speed [Va] | 88 kts |
| Normal Operating Speed [Vno] | 110 kts |
| Never Exceed Speed [Vne] | 145 kts |