Let L-410 Private Charter Flights and Prices
Development of the L-410 was started in the 1960s by the Czechoslovak aircraft manufacturer Let Kunovice. The first prototype flew on April 16, 1969. Due to delays, the prototype and first production version were powered by Pratt & Whitney Canada PT6A-27 engines. The L-410UVP-E (the most common variant of the L-410) has a take-off weight to 6400 kg, M601E engines with increased power, new five-blade propellers designated V 510 and wing tip tanks to increase fuel quantity.
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Aircraft Size
| Aircraft Size | English | Metric |
|---|---|---|
| Length | 47.31 ft | 14.42 m |
| Wing Span | 65.55 ft | 19.98 m |
| Height | 19.13 ft | 5.83 m |
| Bag. Capacity | 48 ft³ | 1 m³ |
Cabin Size
| Cabin Size | English | Metric |
|---|---|---|
| Length | 18.33 ft | 5.59 m |
| Width | 6.43 ft | 1.96 m |
| Height | 5.45 ft | 1.66 m |
| Area | 632 ft³ | 18 m³ |
Aircraft Seats
| Layout | Seats |
|---|---|
| Max Seating | 19 |
| Typical Seating | 19 |
| Pilots | 2 |
Average Prices
| Costs | USD | EUR |
|---|---|---|
| Purchase New | - | - |
| Purchase Used | - | - |
| Charter Rate | 3,000 USD/hour | 3,000 EUR/hour |
Performance Specifications
| Performance | English | Metric |
|---|---|---|
| IFR Range | 1,134 nm | 2,100 km |
| Cruise Speed | 216 KTAS | 400 km/h |
| Certified Ceiling | 20,721 ft | 6,316 m |
| Rate of Climb | 1,416 ft/m | 432 m/m |
| Takeoff Distance | 2,246 ft | 685 m |
| Landing Distance | 1,574 ft | 480 m |
| Max Takeoff Weight | 14,112 lbs | 6,401 kg |
| Max Landing Weight | 13,671 lbs | 6,201 kg |
| Useful Weight | 5,325 lbs | 2,415 kg |
| Payload with Full Fuel | 3,968 lbs | 1,800 kg |
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