FORCETALLY
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At a glance
Eurocopter EC130larger figure on 2 of 7
Kazan Ansatlarger figure on 5 of 7
Measured figures
Length
Single source12.64m (41ft 6 in)[source]
Length
Single sourceConfiguration
| Specification | Eurocopter EC130 | Kazan Ansat |
|---|---|---|
| Type | Light utility helicopter[source] | Multipurpose utility helicopter[source] |
| National origin | France Germany Europe[source] | Russia[source] |
| Manufacturer | Eurocopter Airbus Helicopters[source] | Kazan Helicopters[source] |
| Status | In production[source] | In service |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
13.76 m (45 ft 2 in)[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; Empty weight
Single sourceMaximum take-off; Max takeoff weight
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]
2 × Pratt & Whitney Canada PW207K turboshaft engines (630 shp) each
Single source2 × Pratt & Whitney Canada PW207K turboshaft engines, 470 kW (630 shp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 1000[source] | — |
|---|
| Manufactured | 1999–present[source] | 1998–present[source] |
|---|
| Introduction date | 2001[source] | 28 August 2013[source] |
|---|
| First flight | 24 June 1999[source] | 17 August 1999[source] |
|---|
| Developed from | Eurocopter AS350 Écureuil[source] | — |
|---|
| Capacity | 5-6 (1 pilot)[source] | **7–8 passengers 2 stretchers and 3 attendants 1,235 kg (2,723 lb) internal[source] |
|---|
| Fuel capacity | 540 L (140 US gal; 120 imp gal)[source] | 535 kg[source] |
|---|
| Primary user | — | Russian Aerospace Forces[source] |
|---|
| Main rotor area | — | 103.87 m 2 (1,118.0 sq ft)[source] |
|---|
| Never exceed speed | — | 275 km/h (171 mph, 148 kn)[source] |
|---|
| Hover ceiling OGE | — | 4,396 ft (1,340 m)[source] |
|---|