Description
The Mi-8T transport helicopter is a versatile aircraft that has proven itself in a wide range of civilian applications. Its spacious cabin and flexible design make it well suited for a variety of missions, and its reliability and durability have made it a popular choice for challenging environments.
With more than 17,000 units produced to date, the Mi-8T is one of the most widely used helicopters in the world. Its enduring popularity is testament to its versatility and effectiveness as a transport platform. Whether carrying cargo or passengers, or performing specialized tasks such as firefighting or medical evacuation, the Mi-8T remains an important part of many organizations’ fleets.
- According to the General Designer’s recommendations of the Supplier has the right to change the mentioned the quality of the vendor items and aggregates installed on the helicopter with the prior agreement with the Customer.
- The Supplier reserves the right to replace the specified items with equivalent ones, with same or better technical and operational characteristics than those above listed with the prior agreement with the Customer.
Characteristics
Length
59.61 ft (18,17 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
161 mph (260 kph)
Cruising speed
143 mph (230 kph)
Practical flight range
323 mi (520 km)
Theoretical ceiling
6,234 ft (1900 m)
Practical ceiling
14,763 ft (4500 m)
Payload in the cabin
8,818 lb (4000 kg)
Payload on the suspension
6,613 lb (3000 kg)
Specification
Powerplant and transmission
Temperature control
URT-27-5s
Main rotor hub
8-1930-000 ver.2
Tail rotor drive shaft
8A-1516-000
Tail gear box
246-1517-000
Intermediate gear box
8A-1515-000
Fan drive cardan shaft
8A-6314-00
Electric centrifugal pump
ECN-75B
Electric centrifugal pump
ECN-40
Fuel shut-off valve, details:
768600MA
• Electric actuator
EPV-150MT ver.2
Control and hydraulic system
Tail rotor
8-3904-000 ver.06
Main rotor blades
8AT.2710.000
Hydraulicf ilter
8D2.966.017-2
Lock-out valve
GA-172-00-2/T
Solenoid valve
GA-192/2 or GA-192/T
Emergency power supply valve
GA-59/1
Pump relief valve, automatic
GA-77V
Solenoid operated two-position valve
GA-74M/5
Installation of hydraulic amplifiers with support arms 8АТ-5104-305
8AMT-5104-200
Airframe, landing gear and pneumatic equipment
Main L.G. shock strut
8A-4101-00B-1
Main L.G. shock strut
8A-4101-00B-2
Nose L.G. shock strut
8A-4201-00A
Pneumatic control unit
UPO3/2M
Tire of main LG
865×280 mod.1A
Tire of main LG
595×185 mod.14
Pressure reducing valve
UP03/2M
Heated windshield
V8BP.000
Tail bumper shock strut
V24-4301-100-7
Fire extinguishing, anti-icing, heating and air conditioning equipment
Fire detection and warning system
SSP-FK ver.2
Fire extinguisher, details:
VP-7400-200
• Valve fire extinguisher squib control head
GZSM
Control shutter, details:
1919T
• Electric actuator
EPV-50BT ver.2
• Rotor slip ring
8AT-7411
• Rotor slip ring
8AT-7420
Electrical and commutation equipment
Integrated device
DMR-600T-4
Windscreen wiper electric actuator /
EPK-2T-60
Static inverter
PO-750-2s
Programming mechanism box
PMK-21
Step down, transformer
TP-115/36
Temperature regulator
TER-1M
Transformer
TF 1-25.50-100
Search / landing light composed, details:
MPRF-1M
• Lamp-light
LFS-PR27-200+130
• Beacon alarm lamp
MSL-3 2s
• Forward navigation light
BANO-64
• Tail light
HS-62 (HS-39)
Engines and gear box monitoring equipment
Three-pointer electric indicator
UI3-3K
Three-pointer electric indicator
UI3-6K
Inductive pressure unit
ID-8
Resistance thermometer detector head
P-1
Small-size inductive indicator
ID-100
Multipurpose electric resistance thermometer
TUE-48
Tachometer indicator
ITE-1
Pressure switch heat
MSTV-2.5S
Flight and navigation equipment
Compass system, details:
GMK-1A
• Autopilot composed of:
AP-34B ver.2
• Control panel
6S2.390.007-3
• Control unit
6S2.399.000
• Force-balance transducers
6S2.553.002
• Rate gyro
DUS 1209E, G, K
• Altitude controller
KV-11
• Amplifiers block
BUNPP-V ver.1
• Operational status signal unit
BSG
• Erecting cut-out switch
VK-53E-RV
• Rate-of-climb indicator
VAR-10MK ver.4
• Liquid magnetic compass
KI-13K
• Pitot-statictube
PVD-6M
• Altimeter
VD-10VK ver.2
• Speed indicator
US-450K ver.2
• Indicator
UGR-4UK ver.3
Fuel, hydraulic, pneumatic and electric systems monitoring equipment
Aviation electrical kerosene meter
SKES-2027B
One-point erelectric indicator
UI1-100K
Pressure sensor inductive (of DIM-100K)
ID-100
Electric thermometer indicator
TV-1
Flight data recorder of:
BUR-1-2ZH
• Protected recorder unit
ZBN
• Angular displacement transmitter
MU-615A ver.1
• Altitude transmitter
DV-15MV ver.2
• DC external power socket
SHRAP-500K
Radio navigation equipment
Automatic direction finder
ARK-9
Radio altimeter
RV-3 lit.3
Radio communication equipment
Intercommunication system
SPU-7
Voice information reporting system
RI-65B