Credit
Ronnie Robertson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
EC175 · rotors running
Single source18.06 m (59 ft 3 in) rotors running[source]
EC155 B1 · Length
Configuration
| Specification | Airbus Helicopters H175 | Eurocopter EC155 |
|---|---|---|
| Type | Medium utility helicopter[source] | Passenger transport helicopter[source] |
| National origin | Multinational[source] | Multinational[source] |
| Manufacturer | Eurocopter Airbus Helicopters Aviation Industry Corporation of China[source] | Eurocopter Airbus Helicopters[source] |
| Status | In service[source] |
14.3 m (46 ft 11 in)[source]
Empty; EC175 · Empty weight
Single sourceGross; EC175 · Gross weight
Single sourceMaximum take-off; EC175 · Max takeoff weight
Single source4,603 kg (10,148 lb)[source]
7,500 kg (16,535 lb)[source]
7,800 kg (17,196 lb)[source]
Empty; EC155 B1 · Empty weight
Single sourceGross; EC155 B1 · Gross weight
Single sourceEC175 · 2 × Pratt & Whitney Canada PT6C-67E turboshaft engines with dual channel FADEC each for take-off
Single source2 × Pratt & Whitney Canada PT6C-67E turboshaft engines with dual channel FADEC, 1,324 kW (1,776 hp) each for take-off[source]
EC155 B1 · 2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power each
Single source2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power, 697 kW (935 hp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Active[source] |
| Manufactured | 2009–present[source] | 1997–present[source] |
|---|
| Introduction date | H175 : December 2014[source] | March 1999[source] |
|---|
| First flight | H175: 17 December 2009 AC352: 20 December 2016[source] | 17 June 1997[source] |
|---|
| Capacity | 12-18 pax[source] up to 18 passengers[source] | 13 passengers or 2,301 kg (5,073 lb) payload[source] |
|---|
| Fuel capacity | 2,710 L (720 US gal; 600 imp gal) / 2,136 kg (4,709 lb)[source] | — |
|---|
| Main rotor area | 172 m 2 (1,850 sq ft)[source] | 124.7 m 2 (1,342 sq ft)[source] |
|---|
| Developed from | — | Eurocopter AS365 Dauphin[source] |
|---|
| Variant | — | KAI LCH[source] |
|---|
| Developed into | — | Eurocopter X³ KAI LAH-1 Miron[source] |
|---|
| Never exceed speed | — | 324 km/h (201 mph, 175 kn)[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; EC155 B1 · Max takeoff weight
Single source