The Let-410 Turbolet is a twin engined short-range transport aircraft. This aircraft has made a name for itself on the continent with its remarkable "hot and high" performance, excellent STOL capabilities, durable structure and ability to operate under extreme climatic conditions.

General characteristics		Performance
Crew: 2 (pilot, co-pilot)		Maximum speed: 388 km/h (210 knots, 241 mph)
Capacity: 19 passengers or 1,710 kg of cargo		Cruise speed: 311 km/h (168 knots, 194 mph)
Length: 14.42 m (47 ft 4 in)		Range: 1,040 km (562 nm, 646 mi)
Wingspan: 19.48 m (63 ft 11 in)		Range: 1,040 km (562 nm, 646 mi)
Height: 5.83 m (19 ft 1 1/2 in)		Service ceiling 7,000 m (22,960 ft)
Wing area: 35.18 m² (378.5 ft²)		Rate of climb: 468 m/min (90 m/min with one engine)
Empty weight: 3,725 kg (8,195 lb)		(1,535 ft/min)
Loaded weight: 5,800 kg (12,760 lb)
Max takeoff weight: 6,400 kg (14,520 lb)
Powerplant: 2× Walter M601E turboprop engines,
560 kW (750 hp) each