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.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

Aircraft status: Status unknown

Configuration

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)

Overall Dimensions

Data on aircraft size

Overall Height: 3.97 m (13.0 ft)

Overall Length: 21.35 m (70.0 ft)

Overall Width: 17.30 m (56.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Motor Sich TV3-117VMA turbine

Engine manufacturer: Motor Sich

Take-off / rated power: 1640 kW (2198 hp)

Intermediate power: 1618 kW (2169 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 11500 kg (25353 lb)

Max Range: 440 km (238 nm)

Max Endurance: 4.0 hrs (4.0 hrs)

Related VFS Resources

Resources related to the Mi-24P , provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the Mi-24P , provided by public sources across the internet.

Images