LE500
LE500 is a light 4 - 5 seat aircraft designed, tested, manufactured and certified strictly according to the CCAR-23-R2 Aviation Regulations. It meets the commercial license training requirements of CCAR-141 for single-engine aircraft pilots training. With modifications, it can be used as a business aircraft, tourism plane, for agriculture and forestry, animal husbandry, fishing and other environmental tasks. It can also be used for air surveying, photography, aviation clubs, private flight, military and paramilitary missions.
FeaturesThe aircraft in its conventional configuration is a low-wing propeller-driven monoplane with a full motion vertical tail, retractable tricycle landing gears and a single piston engine. The aircraft, a single pilot vehicle, has four seats including the pilot’s in its basic version and five for the economic version. There is no optional equipment for the basic version. The service life of its airframe counts up to 10,000 flight hours. The aircraft is designed and certified as per the CCAR-23-R2 requirements for normal category aircrafts. ?Performance ?| Wing Span | 9.879m |
|---|---|
| Overall Length | 7.743m |
| Overall Height | 3.044m |
| Required Take-off Distance | 383 m |
| Required Landing Distance | 270 m |
| Maximum Level Speed | 280Km/h |
| Maximum Cruise Speed | 250Km/h |
| Maximum Rate of Climb | 5.75m/s |
| Ceiling | 4200m |
| Maximum Range | 260 km |
| Maximum Endurance | 8h |
| Maximum Take-off Weight | 1400Kg |
| Payload | 560kg |
| Engine TBO | 2000h |
| Propeller TBO | 2400h |
