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At a glance
Measured figures
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]
1 × Rolls-Royce RR300 turboshaft , 224 shp ( ) continuous, 270 shp (
Single source) takeoff (5 minutes
Single source1 × Rolls-Royce RR300 turboshaft , 224 shp (167 kW) continuous, 270 shp (200 kW) takeoff (5 minutes)[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.
Configuration
| Specification | Enstrom F-28 | Robinson R66 |
|---|---|---|
| Type | Light helicopter[source] | Light utility and trainer helicopter[source] |
| Manufacturer | Enstrom Helicopter Corporation[source] | Robinson Helicopter Company[source] |
| Manufactured | 1965-present[source] | 2007–present[source] |
| Introduction date | 1965[source] | 2010 (FAA certification)[source] |
| Variants | Enstrom TH180 Spitfire Mark I[source] | — |
| Developed into | Enstrom 480[source] | Robinson R88[source] |
| Capacity | two passengers[source] | 4 passengers or 1,200 lb (540 kg) external load[source] |
| Main rotor area | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] | — |
| Country of origin | Vereinigte Staaten[source]Country of design · Entwurfsland | — |
| Designer | — | Frank D. Robinson[source] |
| Status | — | In production, in service[source] |
| Number built | — | 1500 (2024)[source] |
| First flight | — | 7 November 2007[source] |
| Developed from | — | Robinson R44[source] |
| Fuel capacity | — | 73.6 US gallons (279 L)[source] |
| Tail rotor Diameter | — | 5 ft (1.52 m)[source] |
| Never exceed speed | — | 140 kn (160 mph, 260 km/h)[source] |
| Fuel consumption | — | 23 US gallons (87 L) per hour[source] |