Production USA California. This helicopter is designed to carry three passengers with luggage for a distance of 600 kilometers without refueling, cruising speed 200 km / h, maximum altitude 4270 m, the engine Lycoming IO-540 with capacity 260 horsepower, flights are permitted at a temperature of - 30 ° C to 40 ° C, the helicopter is equipped with comfortable seats, intercom, ventilation, heating, quick doors.
Airline Ltd. «AeroGeo» is the manufacturer's service center, performs services for sales, service, rental of light helicopters Robinson R-44.
Russian-made transport helicopter designed for transportation of passengers and cargo MI-8 cargo cabin volume is about 23 square meters with a large cargo hatch, a reinforced floor, cargo and mooring knots etc... The cockpit is equipped with cargo doors and bridges, and, moreover, has a slide door on the left side along the boards set 24 of folding seats.
The helicopters are equipped with external suspension system with load capacity 3000 kg and with a winch onboard boom, which allows up to board the hover cargo weighing up to 150 kg.
The transport version of the cab has a slide door on the left board and the cargo hatch to open doors at the rear of the fuselage. To download a wheel technology, there are stairs with adjustable gauge. Maximum Payload 4000 kg. Maximum speed of 250 km / h, cruising 200 km / h, highest range 900 km, the height of flight to 6000 m.
It has similar characteristics of the Mi-8T, but more on the 1000 kg load capacity as in the fuselage and on the outside of the pendant, in the form "Salon” accommodates 11 or 9 passengers. In this case, the passenger cabin of the helicopter set two tables (one folding), chairs and sofa. In the rear of the cabins are equipped with cloak room and WC.
Russian-made multipurpose helicopter designed to carry passengers and cargo. In the rear of the fuselage is cargo cabin with a door on the left board has dimensions 2,27 x 1,2 x 1,4 m. Container tank is fastened to the floor of the cabin, also it is the point of attachment for the two triple sofas. For other (eighth) passenger to the rear of the shell is mounted folding seat. In the carriage of cargo, passenger seat can be removed. In the health model in the cabin can be fitted to four stretchers, also with available space for the accompanying medical worker. Maximum lifting capacity is 700 kg. Maximum speed of 210 km / h, cruising 190 km / h, highest range 440 km, the height of flight to 4000 m.
The AN-2 is suitable to perform various tasks and can be used, inter alia, the following options: agriculture and transport. The aircraft is equipped with the necessary equipment. There are- the passenger seat, locks and cables to secure cargo, landing ropes, light and sound alarm for drop landing, the handle for attaching sanitary stretchers and wall insulation. Maximum Payload 1500 kg. Cruising speed 180 km / h, highest range 1025 km, the height of flight to 4000 m.
It has similar characteristics of the AN-2, but greater for 300 kg load capacity, a more advanced flight control and navigation equipment, engine running at a distributed aviation fuel TS-1.
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