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]
Mi-38 · excluding rotors
Configuration
| Specification | Airbus Helicopters H175 | Mil Mi-38 |
|---|---|---|
| Type | Medium utility helicopter[source] | Medium transport helicopter[source] |
| National origin | Multinational[source] | Russia[source] |
| Manufacturer | Eurocopter Airbus Helicopters Aviation Industry Corporation of China[source] | Kazan Helicopters[source] |
| Status | In service[source] | In service |
20.282 m (66 ft 7 in) excluding rotors[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]
Gross; Mi-38 · Gross weight
Single sourceMaximum take-off; Mi-38 · Max takeoff 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]
Mi-38 · 2 × Klimov TV7-117 V turboshaft engines each
Single source2 × Klimov TV7-117 V turboshaft engines, 2,100 kW (2,800 hp) each[source]
EC175 · 3,600.0 ft/min
Single source18.288 m/s (3,600.0 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 2009–present[source] | 2003–present[source] |
|---|
| Introduction date | H175 : December 2014[source] | 2 December 2019 (Mi-38T)[source] |
|---|
| First flight | H175: 17 December 2009 AC352: 20 December 2016[source] | 22 December 2003[source] |
|---|
| Capacity | 12-18 pax[source] up to 18 passengers[source] | 30 max / 6,000 kg (13,000 lb) internal payload / 7,000 kg (15,000 lb) external 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] | 349.67 m 2 (3,763.8 sq ft)[source] |
|---|
| Designer | — | Mil Moscow Helicopter Plant[source] |
|---|
| Primary users | — | Russian Air Force Myanmar Air Force[source] |
|---|
| Number built | — | 16 (4 prototypes, 12 serial production units)[source] |
|---|
| Variant | — | Mi-38T[source] |
|---|
| Hover ceiling OGE | — | 3,100 m (10,200 ft)[source] |
|---|
| Disk loading | — | 44.6 kg/m 2 (9.1 lb/sq ft) max[source] |
|---|
| Power/mass | — | 0.1675 kW/kg (0.1019 hp/lb)[source] |
|---|
| Reported operators |
| — |
|---|