The TR-301 aircraft, which was developed on the basis of the An-2 universal aircraft, but with many significantly better characteristics. Can be used from unpaved areas. At approximately the same speeds, payload of 1800 kg, cabin dimensions as the An-2, the TR-301 aircraft: 500 kg lighter than the An-2,
Engine ASh-62TR 1160hp with injection injection, overhaul life is 1000 hours.
consumes AI-95 gasoline,
gasoline consumption is 45% lower than An-2,
oil consumption is reduced by 3 times
one pilot
maintenance as it is, no calendars or resources.

Aircraft specifications:

Maximum takeoff weight - 4600 kg
The empty weight of the aircraft is 2900 kg.
Crew: 1 person
Passenger capacity: up to 12 people.
Maximum speed: 300 km / h
Cruising speed: 170-200 km / h
Service ceiling: 4200 m
Climb rate: up to 6.5 m / s
Take-off run: 400 m
Fuel quantity - 1200 l
Gasoline consumption at cruising speed 100 l / h
Practical range: more than 1800 km.

It is possible to design and manufacture floats.