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]
F28F · Length
Configuration
| Specification | Airbus Helicopters H175 | Enstrom F-28 |
|---|---|---|
| Type | Medium utility helicopter[source] | Light helicopter[source] |
| National origin | Multinational[source] | — |
| Manufacturer | Eurocopter Airbus Helicopters Aviation Industry Corporation of China[source] | Enstrom Helicopter Corporation[source] |
| Status | In service[source] | — |
| Manufactured | 2009–present |
29 ft 3 in (8.92 m)[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; F28F · Empty weight
Single sourceMaximum take-off; F28F · 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]
F28F · 1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine
Single source1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine, 225 hp (168 kW)[source]
F28F · Endurance
Single source3 hr 30 min[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1965-present[source] |
| Introduction date | H175 : December 2014[source] | 1965[source] |
|---|
| First flight | H175: 17 December 2009 AC352: 20 December 2016[source] | — |
|---|
| Capacity | 12-18 pax[source] up to 18 passengers[source] | two 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] | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] |
|---|
| Variants | — | Enstrom TH180 Spitfire Mark I[source] |
|---|
| Developed into | — | Enstrom 480[source] |
|---|
| Country of origin | — | Vereinigte Staaten[source]Country of design · Entwurfsland |
|---|
| Reported operators |
| — |
|---|