The Let L-410 Turbolet is a twin-engine short-range transport aircraft, manufactured by the Czech aircraft manufacturer Let Kunovice, often used as an airliner.
| Role | Regional airliner, cargo aircraft |
|---|---|
| Manufacturer | Let Kunovice |
| First flight | 16 April 1969 |
| Introduction | 1970 |
| Status | In service |
| Produced | 1971–present |
| Number built | 1,200 |
| Variants | Aircraft Industries L 410 NG |
Specifications (L-410 UVP-E20)
General characteristics
- Crew: 2
- Capacity: 19 passengers / 1,800 kg (3,968 lb) payload
- Length: 14.42 m (47 ft 4 in)
- Wingspan: 19.98 m (65 ft 7 in)
- Height: 5.97 m (19 ft 7 in)
- Wing area: 34.86 m2 (375.2 sq ft)
- Aspect ratio: 11.45
- Airfoil: root: NACA 63A418; tip: NACA 63A412
- Empty weight: 4,200 kg (9,259 lb)
- Max takeoff weight: 6,600 kg (14,551 lb)
- Fuel capacity: 1,300 kg (2,866 lb)
- Powerplant: 2 × General Electric H80-200 turboprop engines, 597 kW (801 hp) each
- Propellers: 5-bladed Avia AV 725, 2.3 m (7 ft 7 in) diameter
Performance
- Cruise speed: 405 km/h (252 mph, 219 kn) max cruise
- Range: 510 km (320 mi, 280 nmi) 1,800 kg (3,968 lb) payload, ISA, FL140, 45 min reserve
- Endurance: 5 hours 6 minutes
- Service ceiling: 8,382 m (27,500 ft)
- Rate of climb: 8.5 m/s (1,670 ft/min)
- Fuel consumption: 240 kg/h (529 lb/h)
- Take-off run: 510 m (1,673 ft) (ISA, SL, MTOW)
- Landing run: 500 m (1,640 ft) (ISA, SL, MTOW)
Photo Rob Vogelaar