Bell Helicopter

Manufacturer:

Bell Helicopter

Country:

USA

Commercial designation:

407

Technical designation:

407

Version, Variant:

GX

Type:

Conventional

Currently produced:

Y

Typical missions:

ALL Civil

Flight conditions:

IFR

First flight:

0

Landing system:

skids

Blades number:

4

Tail blades number:

2

MTOW with external loads:

2722 kg

6002.01 lbs

MTOW with only internal loading:

2381 kg

5250.105 lbs

Empty weight:

1242 kg

2738.61 lbs

External payload:

1200 kg

2646 lbs

Internal payload:

1139 kg

2511.495 lbs

Standard fuel tank:

387.2 kg

853.776 lbs

with optionnal external fuel tank:

444.8 kg

980.784 lbs

Cruise speed:

220 km/h

118.8 kt

Maximum cruise speed:

246 km/h

132.84 kt

Vne:

259 km/h

139.86 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

611 km

329.94 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:00:00 h:min

Rate of climb @ SL:

10 m/s

1968 ft/min

Rate of climb @ SL @MTOW:

3.25 m/s

639.6 ft/min

IGE max hovering altitude, MTOW:

1646 m

5398.88 ft

IGE max hovering altitude, empty:

5852 m

19194.56 ft

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

960 m

3148.8 ft

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

4755 m

15596.4 ft

OGE max hovering altitude, MTOW:

1646 m

5398.88 ft

OGE max hovering altitude, empty:

5364 m

17593.92 ft

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

960 m

3148.8 ft

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

4206 m

13795.68 ft

Service ceiling ISA, MTOW:

4892 m

16045.76 ft

Max operating altitude, empty weight:

6096 m

19994.88 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Rolls-Royce

Model:

250-C47B

Engines quantity:

1

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0.315 kg/kW/h

0.5166 lbs/hp/h

Minimum consumption speed @ SL:

111 km/h

59.94 kt

Fuel consumption @ eco cruise speed @SL:

145 kg/h

319.725 lbs/h

Fuel consumption @ min consumption speed @ SL:

95 kg/h

209.475 lbs/h

Engines nominal power:

523 kW

710.757 hp

Transmission shaft max continuous power:

470 kW

638.73 hp

Transmission shaft max power:

503 kW

683.577 hp

Takeoff power 5 min:

606 kW

823.554 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:

12.61 m

41.3608 ft

Rotor diameter:

10.66 m

34.9648 ft

Tail rotor diameter:

1.65 m

5.412 ft

Fuselage length:

10.57 m

34.6696 ft

Overall height:

3.1 m

10.168 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

5 °

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:

6

Average price:

0 $