Airplane TR-410

The TR-410 is a multi-purpose high-wing aircraft with two M-601 turboprop engines based on the L-410 aircraft.

Removed all hydraulics, outdated wiring, electrical equipment, greatly simplified management. The aircraft became 800 kg lighter than the L-410, with a payload capacity of up to 3000 kg. Designed to perform a wide range of aviation tasks in simple weather conditions. Has a certificate of airworthiness.

Flight characteristics of the TR-410 aircraft:

* Maximum takeoff weight-6400 kg

* Empty weight-3100 kg * Crew: 1 person

* Maximum speed: 330 km / h

* Cruising speed: 260-300 km / h.

* Service ceiling: 4200 m

* Rate of climb: up to 8.4 m / s

* Takeoff run: 600 m

* Fuel quantity - 1400 l

* Kerosene consumption at cruising speed - up to 200 kg / h

* Practical range: 1100 km 500 hours warranty

• State: Used

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