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Mi-54  
Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Corporations: Mil Helicopter
Parent System: Mi-54
Initial Operational Capability (IOC):
Total Production: ?
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Description: Mi-54 is a twin-engine, multi-purpose helicopter capable of carrying payloads of up to 1,800 kg externally (1,500 kg internally) or 12-13 passengers. Additionally, the aircraft might assume corporate and VIP transport, search and rescue, border patrol, etc. Its spacious and comfortable cabin (4.25x1.71x1.4 meters) will accommodate 12-13 passengers and a two-man crew. Wide doors, engine dustproof systems, blades anti-icing, and modern avionics are other features introduced by MIL on this aircraft. Mi-54 will be compliant with Russian, FAR-29 and JAR-29 rotary-wing aircraft standards.

MIL Helicopter has not announced yet the engine to power its Mi-54 aircraft. The service ceiling would be 5,500 meters and 2,500 meters out of ground effect. Cruising at 260 kph (top speed of 280 kph) and relying on its internal fuel tanks the Mi-54 would be able to cover ranges of 600 kilometers.

Mi-54 Specifications

Crew: 2
Main Rotor Blades: 4
Number of Engines: 2
Passengers: 12
Dimensions
Height: 3.40 meter (134 inch)
Length: 13.1 meter (517 inch)
Main Rotor Diameter: 13.5 meter (531 inch)
Width: 2.90 meter (114 inch)
Performance
Ceiling: 5,500 meter (18,045 foot)
Max Range: 600 kilometer (324 nautical mile)
Speed
Cruise Speed: 72 mps (259 kph)
Top Speed at High Altitude: 78 mps (152 KTAS)
Weight
Max Takeoff Weight: 4,700 kilogram (10,362 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)
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