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Sunward SA60L-T

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Product description

The Sunward SA60L-T high prototype aircraft (Jingqing series) is based on the Shanhe SA60L light sport aircraft. It is equipped with a turbocharged engine Rotax914. It can reach the maximum take-off power at an altitude of 2450m and the maximum continuous power at an altitude of 4500m, effectively increasing the height of the aircraft. Altitude take-off and landing, climbing performance and high altitude adaptability.

Application: private flight, personnel training, tourism, sports and entertainment, aerial survey and remote sensing, aerial photography

Product parameter

Captain	6.89mm	Take-off speed	85 km/h flap 10°
Horizontal machine height	2.53m	Maximum climb rate	5.5m/s
span	8.6m	Takeoff and run off the ground (altitude 1800)	220 m
Main track	1.79 m	Landing and running stop distance (altitude 1800)	200 m
Empty weight	350 kg	Maneuvering load limit	+4G -2G
Maximum take-off weight	600 kg	Glide ratio	4500 m
Unsurpassable speed	265 km/h	Maximum ceiling	400mm X350mm, can load 20kg
Stall speed	73 km/h flap 45°	Can carry aerial survey/ aerial photography equipment weight	40kg front, 20kg rear
Cruising speed	205 km/h	Device window size	Front opening 500mmX400mm/rear opening 350mmX350mm

Product advantages

Safety

Turbocharged engines can reduce the risk of carburetor icing and improve aircraft safety.

Economy

The cruising speed of the aircraft at high altitude increases and the range is longer. Use unleaded and alcohol-free gasoline for vehicles above RON95, which is easy to use and low operating cost; use 95# unleaded and alcohol-free gasoline for vehicles, one 60-liter fuel tank on each of the left and right wings, full load of 120L, fuel consumption per hour 12 -16 liters, can provide a one-way range of more than 1200km, fuel consumption per 100 kilometers is only about 8 liters

Adaptability

Adopting supercharged engine Rotax914, high-altitude propellers have large pull force and short take-off and landing distances, making the aircraft more applicable in high-altitude areas.

Case show

Hubei Huihong Aerial Survey Machine
Hulunbuir Tianying General Aviation
Liaoning Ruixiang General Aviation
Ningxia Yanchi Airport

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Prototipo alto SA60L-T

Prototipo alto SA60L-T

El prototipo de avión SA60L-T (serie Jingqing) se basa en el avión deportivo ligero Shanhe SA60L. Está equipado con un motor turboalimentado Rotax914. Mejora la entrada de aire del motor, el suministro de combustible y el control del turbocompresor, así c

Caracteristicas

1. Adaptarse al vuelo a gran altitud: equipado con motor turboalimentado Rotax 914 para mejorar el rendimiento general de la aeronave en áreas de gran altitud.

2. Los motores turboalimentados pueden reducir el riesgo de formación de hielo en el carburador y mejorar la seguridad de la aeronave;

3. Todavía puede usar gasolina sin plomo y sin etanol 97 # para vehículos, que es conveniente de usar y de bajo costo operativo;

4. Las hélices de gran altitud tienen una gran fuerza de tracción, distancias cortas de despegue y aterrizaje, y los sitios de mayor altitud son más adaptables;

5. La velocidad de crucero a gran altitud aumenta y el alcance es más largo.

Captain	6.89mm	Take-off speed	85 km/h flap 10°
Horizontal machine height	2.53m	Maximum climb rate	5.5m/s
span	8.6m	Takeoff and run off the ground (altitude 1800)	220 m
Main track	1.79 m	Landing and running stop distance (altitude 1800)	200 m
Empty weight	350 kg	Maneuvering load limit	+4G -2G
Maximum take-off weight	600 kg	Glide ratio
Unsurpassable speed	265 km/h	Maximum ceiling	4500 m
Stall speed	73 km/h flap 45°
Cruising speed	205 km/h