FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Eurocopter EC130larger figure on 4 of 5
HESA Shahed 274larger figure on 1 of 5
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source12.64m (41ft 6 in)[source]
Length
Single sourceConfiguration
| Specification | Eurocopter EC130 | HESA Shahed 274 |
|---|---|---|
| Type | Light utility helicopter[source] | Light utility helicopter[source] |
| National origin | France Germany Europe[source] | Iran[source] |
| Manufacturer | Eurocopter Airbus Helicopters[source] | Iran Aircraft Manufacturing Industrial Company[source] |
| Status | In production[source] | Unknown |
9 m (29 ft 6 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]
1 × Rolls-Royce 250-C20B Turboshaft
Single source1 × Rolls-Royce 250-C20B Turboshaft, 313 kW (420 hp)[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] | At least 3[source] |
|---|
| Manufactured | 1999–present[source] | — |
|---|
| Introduction date | 2001[source] | 30 December 2000[source] |
|---|
| First flight | 24 June 1999[source] | 1997[source] |
|---|
| Developed from | Eurocopter AS350 Écureuil[source] | — |
|---|
| Capacity | 5-6 (1 pilot)[source] | 5 (including pilot)[source] |
|---|
| Fuel capacity | 540 L (140 US gal; 120 imp gal)[source] | — |
|---|
| Designer | — | Institute of Industrial Research and Development of the IRGC[source] |
|---|
| Primary user | — | Islamic Revolutionary Guard Corps[source] |
|---|
| Propellers | — | 2-bladed main and tail[source] |
|---|