Bell Helicopter

Manufacturer:

Bell Helicopter

Country:

USA

Commercial designation:

Jetranger III

Technical designation:

206

Version, Variant:

C20R4

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil ALL

Flight conditions:

First flight:

1977

Landing system:

skids

Blades number:

2

Tail blades number:

0

MTOW with external loads:

1519 kg

3349.395 lbs

MTOW with only internal loading:

1451 kg

3199.455 lbs

Empty weight:

0 kg

0 lbs

External payload:

0 kg

0 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

280 kg

617.4 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

215 km/h

116.1 kt

Maximum cruise speed:

224 km/h

120.96 kt

Vne:

241 km/h

130.14 kt

Max negative g @ MTOW:

0.5 g

Max positive g @ MTOW:

3.5 g

Range with normal tanks:

700 km

378 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

0 m

0 ft

IGE max hovering altitude, empty:

6100 m

20008 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

0 m

0 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

6100 m

20008 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-32 °C

-57.6 °F

APU in HC:

Engine manufacturer:

Rolls-Royce Allison

Model:

250-C20R4

Engines quantity:

1

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

283 kW

384.597 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

236 kW

320.724 hp

Takeoff power 5 min:

335 kW

455.265 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

11.9 m

39.032 ft

Rotor diameter:

10.16 m

33.3248 ft

Tail rotor diameter:

1.58 m

5.1824 ft

Fuselage length:

9.5 m

31.16 ft

Overall height:

3.05 m

10.004 ft

Main rotor blades chord:

0.33 m

1.0824 ft

Tail rotor blades chord:

0.13 m

0.4264 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

1

Max pax number:

4

Average price:

353000 $