Eurocopter

Manufacturer:

Eurocopter

Country:

Europe

Commercial designation:

Lakota

Technical designation:

UH-72

Version, Variant:

A

Type:

Conventional

Currently produced:

N

Typical missions:

Military Utility

Flight conditions:

IFR

First flight:

2007

Landing system:

skids

Blades number:

4

Tail blades number:

2

MTOW with external loads:

3585 kg

7904.925 lbs

MTOW with only internal loading:

3585 kg

7904.925 lbs

Empty weight:

1792 kg

3951.36 lbs

External payload:

1500 kg

3307.5 lbs

Internal payload:

1793 kg

3953.565 lbs

Standard fuel tank:

694 kg

1530.27 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

240 km/h

129.6 kt

Maximum cruise speed:

246 km/h

132.84 kt

Vne:

0 km/h

0 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

680 km

367.2 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

8.1 m/s

1594.08 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3445 m

11299.6 ft

IGE max hovering altitude, empty:

0 m

0 ft

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

3445 m

11299.6 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:

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:

0 m

0 ft

Max operating altitude, empty weight:

5485 m

17990.8 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-45 °C

-81 °F

APU in HC:

Engine manufacturer:

Turbomeca

Model:

Arriel 1E2

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:

0 kW

0 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

0 kW

0 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

574 kW

780.066 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:

13 m

42.64 ft

Rotor diameter:

11 m

36.08 ft

Tail rotor diameter:

1.96 m

6.4288 ft

Fuselage length:

10.2 m

33.456 ft

Overall height:

3.96 m

12.9888 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:

87 dB EPNL

Noise at flyover, limit:

94 dB EPNL

Noise at takeoff, level:

88 dB EPNL

Noise at takeoff, limit:

95 dB EPNL

Noise at landing, level:

91 dB EPNL

Noise at landing, limit:

96 dB EPNL

Crew:

1

Max pax number:

9

Average price:

0 $