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tags:

aircraft

Manufacturer:

Country:

Commercial designation:

Technical designation:

Version, Variant:

Type:

Currently produced:

Typical missions:

Flight conditions:

First flight:

Landing system:

Blades number:

Tail blades number:

weight

MTOW with external loads:

kg

0 lbs

MTOW with only internal loading:

kg

0 lbs

Empty weight:

kg

0 lbs

External payload:

kg

0 lbs

Internal payload:

kg

0 lbs

Standard fuel tank:

kg

0 lbs

with optionnal external fuel tank:

kg

0 lbs

performance

Cruise speed:

km/h

0 kt

Maximum cruise speed:

km/h

0 kt

Vne:

km/h

0 kt

Max negative g @ MTOW:

g

Max positive g @ MTOW:

g

Range with normal tanks:

km

0 nm

Max range with auxiliary external tanks:

km

0 nm

Max endurance @ min consumption speed:

h:min

Rate of climb @ SL:

m/s

0 ft/min

Rate of climb @ SL @MTOW:

m/s

0 ft/min

IGE max hovering altitude, MTOW:

m

0 ft

IGE max hovering altitude, empty:

m

0 ft

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

m

0 ft

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

m

0 ft

OGE max hovering altitude, MTOW:

m

0 ft

OGE max hovering altitude, empty:

m

0 ft

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

m

0 ft

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

m

0 ft

Service ceiling ISA, MTOW:

m

0 ft

Max operating altitude, empty weight:

m

0 ft

Highest use Temperature:

°C

0 °F

Lowest use Temperature:

°C

0 °F

power

APU in HC:

Engine manufacturer:

Model:

Engines quantity:

Powerplant category:

Main rotor rotation speed:

rpm

Fuel consumption @ SL @ max continuous speed:

kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

kg/h

0 lbs/h

Engines nominal power:

kW

0 hp

Transmission shaft max continuous power:

kW

0 hp

Transmission shaft max power:

kW

0 hp

Takeoff power 5 min:

kW

0 hp

OEI 30s power:

kW

0 hp

OEI 2min power:

kW

0 hp

OEI max continuous power :

kW

0 hp

OEI max continuous transmission power:

kW

0 hp

OEI 30 sec transmission power:

kW

0 hp

OEI 2 min transmission power:

kW

0 hp

dimensions

Overall length:

m

0 ft

Rotor diameter:

m

0 ft

Tail rotor diameter:

m

0 ft

Fuselage length:

m

0 ft

Overall height:

m

0 ft

Main rotor blades chord:

m

0 ft

Tail rotor blades chord:

m

0 ft

Mast tilt angle:

°

noise

Noise at flyover, level:

dB EPNL

Noise at flyover, limit:

dB EPNL

Noise at takeoff, level:

dB EPNL

Noise at takeoff, limit:

dB EPNL

Noise at landing, level:

dB EPNL

Noise at landing, limit:

dB EPNL

crew and pax

Crew:

Max pax number:

use

Average price:

$