Airplane TR-410

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

All hydraulics, outdated electrical wiring, and electrical equipment were removed, and control was significantly simplified. The aircraft became 800 kg lighter than the L-410, with a carrying capacity of up to 3000 kg. Designed to perform a wide range of aviation tasks in simple weather conditions. Has an airworthiness certificate.

Flight characteristics of the TR-410 aircraft:

* Maximum take-off 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

* Climbing rate: up to 8.4 m/s

* Takeoff length: 600 m

* Fuel quantity - 1400 l

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

* Practical range: 1100 km 500 hours warranty

Photo: pkk-tr.ru.

• State: Used

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