FORCETALLY
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At a glance
Measured figures
Length
Single source12.64m (41ft 6 in)[source]
Mi-10 · fuselage only
Single sourceConfiguration
| Specification | Eurocopter EC130 | Mil Mi-10 |
|---|---|---|
| Type | Light utility helicopter[source] | Aerial crane[source] |
| National origin | France Germany Europe[source] | Russia[source] |
| Manufacturer | Eurocopter Airbus Helicopters[source] | Mil Moscow Helicopter Plant[source] |
| Status | In production[source] | Active as of 2014 (Mi-10K) |
Mi-10 · overall length, rotors turning
Single source32.86 m (107 ft 10 in) (fuselage only), 41.89 m (137 ft 5 in) (overall length, rotors turning)[source]
Empty; Empty weight
Single sourceMaximum take-off; /
Single sourceMaximum take-off; with external load
Single source1,379kg (3,040 lb)[source]
2,427 kg (5,351 lb) / 2,800 kg (6,173 lb) with external load[source]
Empty; Mi-10 · Empty weight
Single sourceEmpty; Mi-10 · Mi-10K
Single source1 x Turbomeca (now Safran Helicopter Engines) Arriel 2B1 turboshaft engine, 632 kw ( ) takeoff power
Single source1 x Turbomeca (now Safran Helicopter Engines) Arriel 2B1 turboshaft engine, 632 kw (847 hp) takeoff power[source]
Mi-10 · 2 × Soloviev D-25V turboshaft each
Single source2 × Soloviev D-25V turboshaft, 4,100 kW (5,500 hp) each[source]
1,770 ft/min
Single source9.0 m/s (1,770 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 1000[source] | 55[source] |
|---|
| Manufactured | 1999–present[source] | 1964–69[source] |
|---|
| Introduction date | 2001[source] | 1963[source] |
|---|
| First flight | 24 June 1999[source] | 15 June 1960[source] |
|---|
| Developed from | Eurocopter AS350 Écureuil[source] | Mil Mi-6[source] |
|---|
| Capacity | 5-6 (1 pilot)[source] | 28 passengers or 3 t (3,000 kg; 6,600 lb) internally up to 15 t (15,000 kg; 33,000 lb) payload on platform or 8 t (8,000 kg; 18,000 lb) max slung payload[source] |
|---|
| Fuel capacity | 540 L (140 US gal; 120 imp gal)[source] | — |
|---|
| Ground clearance under fuselage | — | 3.75 m (12 ft 4 in)[source] |
|---|
| Main rotor area | — | 962 m 2 (10,350 sq ft)[source] |
|---|
| Hovering ceiling out of ground effect | — | 3,000 m (9,840 ft)[source] |
|---|
Gross; Mi-10 · Gross weight
Single sourceGross; Mi-10 · Mi-10K
Single sourceMaximum take-off; Mi-10 · Max takeoff weight
Single sourceMaximum take-off; Mi-10 · Mi-10K
Single source