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Bell Helicopter

407

tags: ALL Civil
Bell Helicopter 407 407

aircraft

Manufacturer:

Bell Helicopter

Country:

USA

Commercial designation:

407

Technical designation:

407

Version, Variant:

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

weight

MTOW with external loads:

2722 kg

6002.01 lbs

MTOW with only internal loading:

2381 kg

5250.105 lbs

Empty weight:

1210 kg

2668.05 lbs

External payload:

1200 kg

2646 lbs

Internal payload:

1171 kg

2582.055 lbs

Standard fuel tank:

387.2 kg

853.776 lbs

with optionnal external fuel tank:

444.8 kg

980.784 lbs

performance

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

power

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

dimensions

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

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 and pax

Crew:

1

Max pax number:

6

use

Average price:

1225000 $

cockpit central panel

Bell Helicopter 407 407

cockpit front panel

Bell Helicopter 407 407

cockpit general

Bell Helicopter 407 407

cockpit steering stick

Bell Helicopter 407 407

cockpit collective

Bell Helicopter 407 407

from above

Bell Helicopter 407 407

from below

Bell Helicopter 407 407

front side

Bell Helicopter 407 407

left side

Bell Helicopter 407 407

rear side

Bell Helicopter 407 407

right side

Bell Helicopter 407 407