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]
S-92 · Length
Configuration
| Specification | Airbus Helicopters H175 | Sikorsky S-92 |
|---|---|---|
| Type | Medium utility helicopter[source] | Medium-lift transport/utility helicopter[source] |
| National origin | Multinational[source] | United States[source] |
| Manufacturer | Eurocopter Airbus Helicopters Aviation Industry Corporation of China[source] | Sikorsky Aircraft[source] |
| Status | In service[source] | In service |
68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[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; S-92 · Empty weight
Single sourceGross; S-92 · 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]
S-92 · 2 × General Electric CT7-8A turboshaft engines, 2,520 shp ( ) each
Single source2 × General Electric CT7-8A turboshaft engines, 2,520 shp (1,880 kW) 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] | 1998–present[source] |
|---|
| Introduction date | H175 : December 2014[source] | 2004[source] |
|---|
| First flight | H175: 17 December 2009 AC352: 20 December 2016[source] | December 23, 1998[source] |
|---|
| Capacity | 12-18 pax[source] up to 18 passengers[source] | 19 passengers[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] | 2,492.3 sq ft (231.54 m 2 )[source] |
|---|
| Primary users | — | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
|---|
| Number built | — | at least 300[source] |
|---|
| Developed from | — | Sikorsky S-70[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[source] |
|---|
| Cabin dimensions | — | 20 ft (6 m) long by 6.6 ft (2 m) tall[source] |
|---|
| Blade section | — | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09[source] |
|---|
| Disk loading | — | 9.8 lb/sq ft (48 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.23 hp/lb (0.38 kW/kg)[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source