FORCETALLY
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At a glance
Measured figures
206B Jetranger II · including rotors
Single source38 ft 9.5 in (11.824 m) including rotors[source]
Ka-226T · Length
Configuration
| Specification | Bell 206 | Kamov Ka-226 |
|---|---|---|
| Type | Multipurpose utility helicopter[source] | Light utility[source] |
| National origin | United States / Canada[source] | Russia[source] |
| Manufacturer | Bell Helicopter[source] | Kamov[source] |
| Status | In service[source] | Active[source] |
8.1 m (26 ft 7 in)[source]
Cruise; 206B Jetranger II · at MTOW, 5,000 feet
Single sourceMaximum; 206B Jetranger II · at MTOW (sea level)
Single source122 kn (140 mph, 226 km/h) at MTOW (sea level)[source]
120 kn (140 mph, 220 km/h) at MTOW, 5,000 feet[source]
Cruise; Ka-226T · Cruise speed
Single sourceMaximum; Ka-226T · Maximum speed
Single source206B Jetranger II · 1,350 ft/min (
Single source1,350 ft/min (6.9 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 7,300[source] | 69[source] |
|---|
| Manufactured | 1962–2017[source] | 1996–present[source] |
|---|
| Introduction date | 1967[source] | 2002[source] |
|---|
| First flight | December 8, 1962 (206) January 10, 1966 (206A)[source] | 4 September 1997[source] |
|---|
| Developed from | Bell YOH-4[source] | Kamov Ka-126[source] |
|---|
| Variants | Bell OH-58 Kiowa Bell 407[source] | — |
|---|
| Developed into | Bell 400 TwinRanger[source] | — |
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| Capacity | 4 passengers[source] | Passengers: 7 Cargo: 1,050 kg (2,310 lb) internally, or 1,100 kg (2,400 lb) on an external sling[source] |
|---|
| Fuselage length | 31 ft 2 in (9.50 m)[source] | — |
|---|
| Interior dimensions | 7 ft 2 in (2.18 m) length, by 4 ft 2 in (1.27 m) width, by 4 ft 3 in (1.30 m) height, plus 16 ft 3 (453 L) baggage compartment[source] | — |
|---|
| Main rotor area | 873 sq ft (81.1 m 2 )[source] | — |
|---|
| Blade section | – NACA 0012 mod (11.3%)[source] | — |
|---|
| Maximum speed at 5,000 ft | 116 kn (133 mph; 215 km/h) at MTOW[source] | — |
|---|
| Disk loading | 4 lb/sq ft (20 kg/m 2 )[source] | — |
|---|
| Power/mass | 0.09 hp/lb (0.15 kW/kg)[source] | — |
|---|
| Primary user | — | Russian Aerospace Forces[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] |
|---|