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]
IAR 316 · Length
Configuration
| Specification | Bell 206 | IAR 316 |
|---|---|---|
| Type | Multipurpose utility helicopter[source] | Light utility /training helicopter[source] |
| National origin | United States / Canada[source] | Romania[source] |
| Manufacturer | Bell Helicopter[source] | Industria Aeronautică Română[source] |
| Status | In service[source] | operational for training purposes[source] |
12.82 m (42 ft 1 in)[source]
Empty; 206B Jetranger II · Empty weight
Single sourceMaximum take-off; 206B Jetranger II · Max takeoff weight
Single source1,455 lb (660 kg)[source]
3,200 lb (1,451 kg)[source]
Empty; IAR 316 · Empty weight
Single sourceMaximum take-off; IAR 316 · Max takeoff weight
Single sourceCruise; 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; IAR 316 · Cruise speed
Single sourceMaximum; IAR 316 · Maximum speed
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 7,300[source] | 250[source] |
|---|
| Manufactured | 1962–2017[source] | 1971-1987[source] |
|---|
| Introduction date | 1967[source] | 1971[source] |
|---|
| First flight | December 8, 1962 (206) January 10, 1966 (206A)[source] | — |
|---|
| Developed from | Bell YOH-4[source] | Aérospatiale Alouette III[source] |
|---|
| Variants | Bell OH-58 Kiowa Bell 407[source] | — |
|---|
| Developed into | Bell 400 TwinRanger[source] | — |
|---|
| Capacity | 4 passengers[source] | 5 passengers[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] | 95.4 m 2 (1,027 sq ft)[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 | — | Romanian Air Force[source] |
|---|
| Fuel capacity | — | 550 kg (1,210 lb) maximum[source] |
|---|
| Fuselage width | — | 2.6 m (8 ft 6 in)[source] |
|---|
| Hardpoints | — | 2 hardpoints for anti-tank guided missiles[source] |
|---|
| Country of origin | — | Romania[source] |
|---|