FDG50P fixed-wing UAV wingspan of 3.8 meters, fuselage length of 2.58 meters, fuselage weight of 20kg, maximum take-off weight of 60kg, spanning 120~170cc engine, design cruising speed of 100-120km/h, fuel tank 20L, endurance: 10h@3kg payload (20L fuel), 3h@15kg payload, 5h@10kg payload, can be used for aerial photography, surveying and mapping

Specifications

Body length:  2.5m

Wingspan: 3.8m

Maximum take-off weight: 55kg

Maximum payload: 25kg

Endurance: 10h@3kg payload (20L fuel), 3h@15kg payload, 5h@10kg payload,

Flight radius:  200-400km (depending on fuel load)

Maximum control distance remote control (manual control): 1km

Ground station control (depending on the digital transmission distance equipped): standard 30km

Maximum speed:  150km/h

Cruising speed:  90-110km/h

Maximum fuel capacity:  12L/20L (optional)

Maximum operating altitude:  6500m

Maximum wind resistance:  12m/s (level 6 wind)

Operating environment -10℃+45℃; protection against light rain

Engine: 120cc electronic injection inspired one

Power supply battery:  5000mAh-6S lithium battery for engine start

Take-off and landing mode: rolling take-off and landing

GPS positioning system single-point GPS positioning/RTK direction finding (optional)

PNP Oder including 

1 x fixed-wing airframe  Composite Frame(Carbon fiber)

1 x LIRDE 120CC Engine
1 x CW for fixed-wing motor
4 x Servo

1 x Powerboard
1 x Aluminum box (1860*840*830MM)