The Mi-8 is a multifunctional helicopter, the scope of which is expanding due to constant modernization and the possibility of equipping it with a large number of additional devices for various tasks. The helicopter can be used under a wide variety of conditions and temperatures (from -50 to +50 degrees Celsius) and is easy to operate and maintain.

The development of the V-8 (Mi-8) helicopter began at the M.L. Mil (now OJSC "Moscow Helicopter Plant, named after ML Mil", part of the holding "Russian Helicopters") replaced the tried and tested multipurpose piston helicopter Mi-4 in May 1960. The Mi-8 was developed as a profound modernization of the Mi-4 with a gas turbine engine. The helicopter was developed simultaneously in two versions: Passenger Mi-8P and Transport Mi-8T.

In the meantime, don't worry. "

FLIGHT FEATURES OF THE MI-8T
Crew 3 people

Top speed - 250 km / h

Cruising speed at normal flight weight - 220 km / h

Maximum flight altitude with passengers - 3000 m

Flight range in the transport version without additional fuel tanks - 450 km

Maximum takeoff weight - 12,000 kg

Maximum payload - 4000 kg

Maximum loading weight of the outer sling - 3000 kg

Максимальный вес груза, поднимаемый бортовой стрелой - 150 кг

The Mi-8 HP helicopter has a comfortable cabin for 14 passengers. It has two doors with folding ladders.

In the meantime, don't worry. "

FLIGHT CHARACTERISTICS OF MI-8PS
In the meantime, don't worry. "
Crew 3 people

Top speed - 250 km / h

Cruising speed at normal flight weight - 220 km / h

Maximum flight altitude with passengers - 3000 m

Flight range in the transport version without additional fuel tanks - 450 km

Maximum takeoff weight - 12,000 kg

Maximum payload - 4000 kg

Maximum load weight on the outer sling - 3000 kg

Максимальный вес груза, поднимаемый бортовой стрелой - 150 кг

The light multi-purpose aircraft An-26 for military transport is designed for the transport of cargo over short and medium-haul routes. It can be used to carry passengers on folding seats along the side.

An-26 - basic modification.

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AN-26 PERFORMANCE CHARACTERISTICS

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Wingspan 29.2 m;
Aircraft length 23.8 m;
Height 8.6 m;
Wing area 75.0 m2.
Crew of 5 people.
The An-26 aircraft can carry 38-40 passengers or 30 paratroopers or 24 wounded with medical attendants.

Weights and loads:

Maximum start 24,000 kg,
Normal start 23000 kg,
Empty 15020 kg;
Fuel 5500 kg;
Maximum payload 5500 kg.
Flight data:
Top speed 540 km / h;
Cruising speed 435 km / h;
Landing speed 190 km / h;
practical ceiling 7500 m;
practical area:
- with a maximum load of 1240 km (according to other sources 1100 km),
- with a maximum fuel supply (ferry) 2660 km,
Start run 780 m (according to other sources 870 m),

длина пробега 730 м (по другим данным 650 м).