Eurocopter

Manufacturer:

Eurocopter

Country:

Europe

Commercial designation:

Tiger

Technical designation:

EC665

Version, Variant:

UHT

Type:

Conventional

Currently produced:

N

Typical missions:

Military Combat Attack

Flight conditions:

IFR

First flight:

1991

Landing system:

wheels

Blades number:

4

Tail blades number:

3

MTOW with external loads:

6100 kg

13450.5 lbs

MTOW with only internal loading:

0 kg

0 lbs

Empty weight:

4350 kg

9591.75 lbs

External payload:

1650 kg

3638.25 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

1105 kg

2436.525 lbs

with optionnal external fuel tank:

1689 kg

3724.245 lbs

Cruise speed:

230 km/h

124.2 kt

Maximum cruise speed:

259 km/h

139.86 kt

Vne:

298 km/h

160.92 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

800 km

432 nm

Max range with auxiliary external tanks:

1280 km

691.2 nm

Max endurance @ min consumption speed:

03:25:00 h:min

Rate of climb @ SL:

10.7 m/s

2105.76 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:

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:

3200 m

10496 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:

4000 m

13120 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

35 °C

63 °F

Lowest use Temperature:

-30 °C

-54 °F

APU in HC:

Engine manufacturer:

Turbomeca

Model:

MTR 390

Engines quantity:

2

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:

1746 kW

2372.814 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

1936 kW

2631.024 hp

OEI 30s power:

1160 kW

1576.44 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:

15.82 m

51.8896 ft

Rotor diameter:

13 m

42.64 ft

Tail rotor diameter:

2.7 m

8.856 ft

Fuselage length:

14.27 m

46.8056 ft

Overall height:

5.2 m

17.056 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:

2

Max pax number:

0

Average price:

32000000 $