1990 Mi-8T Transport

Year: 1990
Total Time: 1476
Notes: requires overhaul

The Mi-8T transport helicopter is designed for delivery of cargo inside the cargo cabin, as well as for transportation of oversized cargo on an external sling weighing up to 6,600 pounds (3 tons) and a winch up to 330 pounds (150 kg). Mi-8T is used for construction and installation and other work in hard-to-reach areas and facilities.

$300,000

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Mi-8T (transport) 1990, requires overhaul, 1476 hours
  • Mi-8T (transport) 1990, requires overhaul, 1476 hours
  • Mi-8T (transport) 1990, requires overhaul
  • Mi-8 Helicopter Drawing

Description

Medium multi-purpose transport helicopter Mi-8T has unique flight and technical and operational characteristics. High reliability, ease of operation and maintenance, convenience of the helicopter operation allowed it to become popular all over the world.

In the standard configuration the transport version of the helicopter is designed for cargo and passenger transportation. In case of need the helicopter can be equipped with additional fuel tanks, removable equipment and can be used for firefighting, search and rescue operations, aerial photography and other operations.

The rugged and large cargo cabin is designed to carry a variety of cargo configurations, with a total volume of up to 23 cubic meters. There is a large hatch at the rear and a sliding door on the left side for easy loading. The cab has removable folding seats for 22 passengers.

For protection against icing the main and tail rotor blades and cockpit windows are equipped with electro-thermal anti-icing system.

Due to the helicopter design and equipment it can be operated at autonomous bases and unequipped sites.

Characteristics

Length
59.61 ft (18,17 m)
Height
18.53 ft (5,65 m)
Diameter of the main rotor
69.84 ft (21,29 m)
Tail rotor diameter
12.82 ft (3,91 m)
Empty helicopter weight
14,605 lb (6625 kg)
Normal take-off weight
24,471 lb (11100 kg)
Maximum take-off weight
26,455 lb (12000 kg)
Engines
TV2-117AG (Klimov) x 2
Rated power
1,257 kWt x 2
Take-off power
1,500 kWt x 2
Maximum power
1,620 kWt x 2
Maximum speed
155 mph (250 kph)
Cruising speed
140 mph (225 kph)
Practical flight range
300 mi (480 km)
Theoretical ceiling
6,234 ft (1900 m)
Practical ceiling
14,763 ft (4500 m)
Crew
2+1
Payload in the cabin
8,818 lb (4000 kg)
Payload on the suspension
6,613 lb (3000 kg)

Specification

Engine LH
TV2-117AG
Engine RH
TV2-117AG
Main Gearbox
VR-8A
Main rotor hub
8-1930-000 PS
Swash plate
8-1950-000 PS
Cooling Fan
8A-6311-00 PS
Tail gearbox
246-1517-000 PS
Intermediate gearbox
8A-1515-000 PS
Hydraulic booster
KAU-30B-000 PS
Hydraulic booster
RA60B-000 PS
Tail rotor blade
246-3922-00 PS
Main rotor blade
8AT.2710.00 PS
Tail rotor blade
8A-1516-000 PS
Tail rotor hub
246-3904-000 PS
Gimbal shaft
8A-6314-00 PS
Actuator portion
8AT-5104-200 PS
Generator
002 581 PS
Gyro horizon
AGB.00.00.000K PS1
Soft fuel tank
8AT.6101-00 PS
Shock absorber strut left
8A-4101-00B PS
Shock absorber strut right
8A-4101-00B PS
Lever amortization front pillar
8A-4201-00A PS

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