Enstrom

Manufacturer:

Enstrom

Country:

USA

Commercial designation:

480B

Technical designation:

480

Version, Variant:

B

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Law Utility

Flight conditions:

VFR

First flight:

2000

Landing system:

skids

Blades number:

3

Tail blades number:

2

MTOW with external loads:

1361 kg

3001.005 lbs

MTOW with only internal loading:

1361 kg

3001.005 lbs

Empty weight:

826 kg

1821.33 lbs

External payload:

0 kg

0 lbs

Internal payload:

535 kg

1179.675 lbs

Standard fuel tank:

273 kg

601.965 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

213 km/h

115.02 kt

Vne:

231 km/h

124.74 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

684 km

369.36 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:42:00 h:min

Rate of climb @ SL:

8 m/s

1574.4 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

4680 m

15350.4 ft

IGE max hovering altitude, empty:

0 m

0 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:

4200 m

13776 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:

3900 m

12792 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 Allison

Model:

250-C20 W

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:

207 kW

281.313 hp

Transmission shaft max continuous power:

206 kW

279.954 hp

Transmission shaft max power:

227 kW

308.493 hp

Takeoff power 5 min:

227 kW

308.493 hp

OEI 30s power:

313 kW

425.367 hp

OEI 2min power:

313 kW

425.367 hp

OEI max continuous power :

207 kW

281.313 hp

OEI max continuous transmission power:

227 kW

308.493 hp

OEI 30 sec transmission power:

313 kW

425.367 hp

OEI 2 min transmission power:

313 kW

425.367 hp

Overall length:

0 m

0 ft

Rotor diameter:

9.8 m

32.144 ft

Tail rotor diameter:

1.5 m

4.92 ft

Fuselage length:

9.2 m

30.176 ft

Overall height:

3 m

9.84 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 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:

580000 $