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At a glance
Measured figures
F28F · Length
Single source29 ft 3 in (8.92 m)[source]
Ka-226T · Length
Single sourceConfiguration
| Specification | Enstrom F-28 | Kamov Ka-226 |
|---|---|---|
| Type | Light helicopter[source] | Light utility[source] |
| Manufacturer | Enstrom Helicopter Corporation[source] | Kamov[source] |
| Manufactured | 1965-present[source] | 1996–present[source] |
| Introduction date | 1965[source] | 2002[source] |
8.1 m (26 ft 7 in)[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]
Ka-226T · 2 × Turbomeca Arrius 2G1 each
Single source2 × Turbomeca Arrius 2G1 , 432.5 kW (580.0 hp) each[source]
F28F · Endurance
Single source3 hr 30 min[source]
F28F · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Variants | Enstrom TH180 Spitfire Mark I[source] | — |
|---|
| Developed into | Enstrom 480[source] | — |
|---|
| Capacity | two passengers[source] | Passengers: 7 Cargo: 1,050 kg (2,310 lb) internally, or 1,100 kg (2,400 lb) on an external sling[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 | — |
|---|
| National origin | — | Russia[source] |
|---|
| Status | — | Active[source] |
|---|
| Primary user | — | Russian Aerospace Forces[source] |
|---|
| Number built | — | 69[source] |
|---|
| First flight | — | 4 September 1997[source] |
|---|
| Developed from | — | Kamov Ka-126[source] |
|---|
| Passengers | — |
|---|
| Cargo | — | 1,050 kg (2,310 lb) internally, or 1,100 kg (2,400 lb) on an external sling[source] |
|---|
| Hover ceiling | — | 4,600 m (15,100 ft)[source] |
|---|