Variant of the Mil Mi-24 with the NATO designation of 'Hind F'.  The helicopter has a pod and boom configuration, has a passenger capacity of 8, and is fitted with a 30 mm fixed gun mount.  The engines are fitted with deflectors and separators for dust intake prevention.  Onboard equipment allows operation during daytime and twilight under Visual Flight Rules  (VFR) weather conditions.


Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

Aircraft status: Status unknown


Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Tandem

Landing gear: Wheels (all retractable)

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height: 3.97 m 13.0 ft
Overall Length: 21.35 m 70.0 ft
Overall Width: 17.30 m 56.8 ft
Airframe Dimensions
Airframe Length: 17.51 m 57.4 ft
Airframe Width: 6.66 m 21.9 ft
Airframe Height: 3.97 m 13.0 ft
Landing Gear Dimensions
Landing Gear Base: 4.39 m 14.4 ft
Landing Gear Track: 3.03 m 9.9 ft
Cabin Dimensions
Cabin Internal Height: 1.20 m 3.9 ft
Cabin Internal Length: 2.50 m 8.2 ft
Cabin Internal Width: 1.45 m 4.8 ft

Weights and Performance

Data on aircraft weight and flight characteristics

Cruise Speed: 280 km/h

Max Gross Weight (ground): 11,500 kg 25,353 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 11,500 kg 25,353 lb
Empty Weight: 8,500 kg 18,739 lb
Useful Load: 3,000 kg 6,614 lb
Empty Weight Fraction: 0.739
Climb Performance
Max Rate of Climb: 13 m/s 2,461 fpm
Hover Performance
Hover Ceiling IGE:  
Hover Ceiling OGE: 1,500 m 4,921 ft
Max Level Flight Speed: 320 km/h 173 kts
Never Exceed Speed:  
Service Ceiling: 4,500 m 14,764 ft
Range and Endurance
Max Range: 440 km 238 nm
Max Endurance: 4 hrs 4 hrs

Engine Details

Aircraft powerplant (lift and/or propulsion)

Provided powerplant data is for uninstalled, sea level, static operations.

Number of engines: 2
Designation: Motor Sich TV3-117VMA turbine
Manufacturer: Motor Sich
Normal Ratings
Max continuous:  
Take-off / rated: 1640 kW 2198 hp
Intermediate: 1618 kW 2169 hp
OEI Ratings
OEI contingency: 1765 kW 2366 hp
OEI continuous:  
OEI 30-second:  
OEI intermediate: 1618 kW 2169 hp

Primary Lift Device

Data on primary lift devices such as main rotors

Main Rotor Characteristics
Diameter: 17.30 m 56.76 ft
Direction of Rotation: Clockwise
Hub Type:
Main Rotor Blade Characteristics
Blade Construction: Aluminum alloy spar, honeycomb core
Blade Chord: 0.580 m 1.90 ft
Blade Tip Geometry: Conventional
Blade Twist:  
Number of Blades: 5
Main Rotor Derived Characteristics
Disc Area: 235.06 m² 2530.3 ft²
Disc Loading: 48.92 kg/m² 10.020 lb/ft²
Solidity: 0.1067
Main Rotor Blade Derived Characteristics
Blade area per blade: 5.02 m² 54.0 ft²
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Diameter: 3.91 m 12.83 ft
Configuration: Tractor
Direction of Rotation: Top blade aft
Tail Rotor Blade Characteristics
Number of Blades: 3
Blade Construction:  
Blade Chord:  
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area: 12.01 m² 129.2 ft²
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade):  

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