Bell Helicopter

Manufacturer:

Bell Helicopter

Country:

USA

Commercial designation:

Longranger

Technical designation:

206

Version, Variant:

L4

Type:

Conventional

Currently produced:

Y

Typical missions:

VIP Law Utility

Flight conditions:

First flight:

0

Landing system:

skids

Blades number:

2

Tail blades number:

0

MTOW with external loads:

2064 kg

4551.12 lbs

MTOW with only internal loading:

2018 kg

4449.69 lbs

Empty weight:

1039 kg

2290.995 lbs

External payload:

907 kg

1999.935 lbs

Internal payload:

963 kg

2123.415 lbs

Standard fuel tank:

419 kg

923.895 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

205 km/h

110.7 kt

Maximum cruise speed:

230 km/h

124.2 kt

Vne:

241 km/h

130.14 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

600 km

324 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:30:00 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:

5060 m

16596.8 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:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Rolls-Royce

Model:

250-C30P

Engines quantity:

1

Powerplant category:

turbine

Main rotor rotation speed:

394 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

120 km/h

64.8 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

95 kg/h

209.475 lbs/h

Engines nominal power:

325 kW

441.675 hp

Transmission shaft max continuous power:

276 kW

375.084 hp

Transmission shaft max power:

365 kW

496.035 hp

Takeoff power 5 min:

485 kW

659.115 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:

12.92 m

42.3776 ft

Rotor diameter:

11.28 m

36.9984 ft

Tail rotor diameter:

1.65 m

5.412 ft

Fuselage length:

10.56 m

34.6368 ft

Overall height:

3.56 m

11.6768 ft

Main rotor blades chord:

0.3 m

0.984 ft

Tail rotor blades chord:

0.13 m

0.4264 ft

Mast tilt angle:

0 °

Noise at flyover, level:

85 dB EPNL

Noise at flyover, limit:

92 dB EPNL

Noise at takeoff, level:

88 dB EPNL

Noise at takeoff, limit:

93 dB EPNL

Noise at landing, level:

90 dB EPNL

Noise at landing, limit:

94 dB EPNL

Crew:

1

Max pax number:

6

Average price:

1015000 $