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"Soyuz Avia"
They offer services for the rental of helicopters and airplanes to perform aviation work in various directions / air transportation, anywhere in the world.
Mi-8T

Helicopter Mi-8T
Mi-8 is a multifunctional helicopter. The helicopter can be used in a variety of conditions and temperatures (from -50 to +50 degrees Celsius), is easy to operate and maintain.
The development of the V-8 (Mi-8) helicopter began at the Pushkin Museum. Mil (now JSC Mil Moscow Helicopter Plant, part of the Russian Helicopters holding) replaced the proven multi-purpose piston Mi-4 helicopter in May 1960. The Mi-8 was developed as a deep upgrade. Mi-4 with a gas turbine engine. The helicopter was developed simultaneously in two modifications: the passenger Mi-8P and the transport Mi-8T.
In the meantime, there is no need to worry about it. ”
FLIGHT CHARACTERISTICS OF MI-8T
Crew 3 people
The maximum speed is 250 km / h.
Cruising speed at normal flight weight is 220 km / h.
Maximum flight altitude with passengers - 3000 m.
Flight range in transport version without additional fuel tanks is 450 km.
The maximum take-off weight is 12,000 kg.
Maximum payload - 4000 kg
The maximum load weight of the external sling is 3000 kg.
Maximum load weight lifted by side boom - 150 kg
Mi-8MTV

FLIGHT CHARACTERISTICS OF MI-8MTV
Crew, people - 3
Passengers, pers. - 22
Flight range, km-1150
Maximum radius of flight range with return to the point of departure (km) - 575
MASSES AND LOADS
Maximum takeoff weight, kg -13000
Empty helicopter weight, kg - 7200
Maximum load in the cargo compartment, kg - 4000
Maximum load on an external sling, kg -4000
Fuel stock in the main tanks -2600 l (2080 kg)
Fuel supply in the main and additional (internal or external) tanks -4400 l (3520 kg)
FLIGHT DATA
Maximum speed, km / h -250
Cruising speed, km / h -230
Dynamic ceiling, m -6000
MI-8PS

The Mi-8 PS helicopter has a comfortable cabin for 14 passengers. Has two doors with folding ladders.
For now, don't worry. "
FLIGHT CHARACTERISTICS OF MI-8PS
For now, don't worry. "
Crew 3 people
The maximum speed is 250 km / h.
Cruising speed at normal flight weight is 220 km / h.
Maximum flight altitude with passengers - 3000 m.
Flight range in transport version without additional fuel tanks is 450 km.
The maximum take-off weight is 12,000 kg.
Maximum payload - 4000 kg
The maximum load on the external sling is 3000 kg.
Maximum load weight lifted by side boom - 150 kg
MI-26

Flight technical characteristics of the Mi-26
Main rotor diameter, m 32.00
Tail rotor diameter, m 7.61
Length, m 40.03
Height, m 8.145
Width, m 3120
Weight, kg
empty 28000
normal takeoff 49600
maximum takeoff 56000
Engine type 2 GTD ZMKB Progress D-136-2
Power, h.p. 2 x 11650
Maximum speed, km / h 290
Cruising speed, km / h 255
Practical range, km 2000
Range of action, km
with filling the main fuel tanks 800
with filling the main and additional. fuel tanks 1905
Practical ceiling, m 4600
Static ceiling, m 1500
Crew, persons 2 + 1
Payload: up to 120 passengers or 20,000 kg of cargo in the cab or suspended
Modification of the Mi-26T2V
Main rotor diameter, m 32.00
Tail rotor diameter, m 7.61
Length, m 40.03
Height, m 8.145
Width, m 3120
Weight, kg
empty 28000
normal takeoff 49600
maximum takeoff 56000
Engine type 2 GTD ZMKB Progress D-136-2
Power, h.p. 2 x 11650
Maximum speed, km / h 290
Cruising speed, km / h 255
Practical range, km 2000
Range of action, km
with filling the main fuel tanks 800
with filling the main and additional. fuel tanks 1905
Practical ceiling, m 4600
Static ceiling, m 1500
Crew, persons 2 + 1
Payload: up to 120 passengers or 20,000 kg of cargo in the cab or suspended
l-410 NG (Turbolet)

Universal twin-engine aircraft Let L-410 Turbolet
Let L-410 is a nineteen-seat aircraft for local airlines, designed to operate on unprepared unpaved, grassy, snowy areas, as well as on airfields with short runways. Other names: L-410, Let L-410, Turbolet, colloquial names - Cheburashka, Elka, Ellie.
It is planned to launch serial production of the L-410 in Russia on the basis of the Ural Civil Aviation Plant (Yekaterinburg), where a certification check was carried out in order to include the production of the L 410 UVP-E20 aircraft in the list of permitted works to the approval certificate of the production organization.
In the meantime, there is no need to know about it. ”
L-410NG - development of the L-410UVP-E20 + integral wing tanks + almost 2 times more flight range + more powerful engines + increased volume of the front luggage compartment + the cockpit is equipped with the most modern avionics
L-410UVP-E20 specifications:
Crew - 2 pilots
Payload - 19 passengers or 1800 kg cargo
Engine type - 2 × TVD GE H80-200
Takeoff power - 2 × 800 HP
Propeller type - 2 × AVIA AV-725
The number of blades on each propeller - 5
Propellers diameter - 2.3 m
Wingspan - 19.98 m
Plane length - 14.42 m
Aircraft height - 5.83 m
Wing area - 34.86 m2
Empty aircraft weight - 4050 kg
Maximum takeoff weight - 6600 kg
Fuel weight (main tanks) - 1000 kg
Fuel weight (end tanks) - 313.8 kg
Maximum speed - 335 km / h IS
Practical range - 1500 km
Service ceiling - 4200 m
Sale of aircraft
Ми-8Т Санитарный


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Filling and range MI-8T
Ми-8ПС ВИП




TECHNICAL DATA OF MI-8 HELICOPTER
Видео Полетов и Авиационных Работ
Видео Полетов и Авиационных Работ



