FORCETALLY
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At a glance
Measured figures
H160 · Length
Single source13.96 m (45 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | Airbus Helicopters H160 | Eurocopter EC130 |
|---|---|---|
| Type | Medium utility helicopter[source] | Light utility helicopter[source] |
| National origin | Multinational[source] | France Germany Europe[source] |
| Manufacturer | Airbus Helicopters[source] | Eurocopter Airbus Helicopters[source] |
| Status | In production[source] |
12.64m (41ft 6 in)[source]
H160 · Width
Single source3.54 m (11 ft 7 in)[source]
H160 · 2 × Safran Arrano 1A turboshaft engines (1,280 shp) each
Single source2 × Safran Arrano 1A turboshaft engines, 955 kW (1,280 shp) each[source]
1 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]
1,770 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.
In production[source] |
| Manufactured | 2015–present[source] | 1999–present[source] |
|---|
| Introduction date | 2021[source] | 2001[source] |
|---|
| First flight | 13 June 2015[source] | 24 June 1999[source] |
|---|
| Capacity | 12[source] | 5-6 (1 pilot)[source] |
|---|
| Useful load | up to 2,000 kg (4,400 lb)[source] | — |
|---|
| Fuel capacity | 1,120 kg (2,470 lb)[source] | 540 L (140 US gal; 120 imp gal)[source] |
|---|
| Main rotor area | 141 m 2 (1,520 sq ft)[source] | — |
|---|
| Never exceed speed | 315 km/h (196 mph, 170 kn)[source] | — |
|---|
| Disk loading | 42.9 kg/m 2 (8.8 lb/sq ft)[source] | — |
|---|
| Number built | — | 1000[source] |
|---|
| Developed from | — | Eurocopter AS350 Écureuil[source] |
|---|
Maximum take-off; with external load
Single source