Let L-410 Private Jet Charter
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.
Aircraft category
Turboprop Aircraft
Typical Seating
19
Price per hour
3,750
Nautical miles
1134
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.
The average hourly rental rate of the Let L-410 is around 3,750 USD per hour.
The average purchase price of a pre-owned Let L-410 is 3,500,000 USD.
Aircraft Size
Aircraft size | English | Metric |
---|---|---|
Length | 47.32 ft | 14.42 m |
Wing Span | 65.56 ft | 19.98 m |
Height | 19.12 ft | 5.82 m |
Bag. Capacity | 48.38 ft³ | 1.38 m³ |
Cabin Size
Cabin size | English | Metric |
---|---|---|
Length | 18.32 ft | 5.6 m |
Width | 6.42 ft | 1.96 m |
Height | 5.44 ft | 1.66 m |
Area | 632.14 ft³ | 17.9 m³ |
Aircraft Seats
Layout | Seats |
---|---|
Max Seating | 19 |
Typical Seating | 19 |
Pilots | 2 |
Average Prices
Costs | USD | EUR |
---|---|---|
Purchase New | - | - |
Purchase Used | 3,500,000 USD | 3,500,000 EUR |
Hourly rate | 3,750 USD/hour | 3,750 EUR/hour |
Performance Specifications
Performance | English | Metric |
---|---|---|
IFR Range | 1134 nm | 2100 km |
Cruise Speed | 216 KTAS | 400 km/h |
Certified Ceiling | 20721 ft | 6316 m |
Rate of Climb | 1416 ft/m | 432 m/m |
Takeoff Distance | 2246 ft | 685 m |
Landing Distance | 1574 ft | 480 m |
Max Takeoff Weight | 14112 lbs | 6401 kg |
Max Landing Weight | 13671 lbs | 6201 kg |
Useful Weight | 5325 lbs | 2415 kg |
Payload with Full Fuel | 3968 lbs | 1800 kg |