Airbus (Eurocopter) AS365 of n3+

Model Eurocopter Airbus AS 365 N3e able to perform the same functions as the helicopter Eurocopter Airbus AS365 N3+, but has the best flight characteristics for use in hot climates and high altitude and allows the pilot to operate in the improved situational awareness due to the presence of the display parameters of the systems of the helicopter and the engine (VEDM) and a large multifunction display flight control (with digital maps) that will be part of the basic configuration of the helicopter, as well as an updated and expanded list of optional equipment.

Helicopter Eurocopter Airbus AS 365 N3 features excellent performance characteristics that can be used in the harshest operating conditions. This versatile machine is adapted for work in the highlands and hot climate. Thanks to low operating costs it is perfect for most transport problems.

The helicopter has a tail rotor Fenestron type, the use of which has reduced the level of internal and external noise and improve safety. In addition, the machine is equipped with retractable wheeled chassis that enables it to operate in the most busy airports in the world. In the passenger cabin can comfortably accommodate six to eight people. The noise level does not exceed 3.1 dB.

The helicopter is equipped with avionics for flight rules instrument flight (IFR), the autopilot, onboard computer with integrated instrument panel, the so-called glass cockpit.
The new model is equipped with powerful engines Turbomeca Arriel 2C, which raise the car to a height of 3110 m. Eurocopter Airbus AS 365 N3 has a maximum takeoff weight of 4,300 kg maximum payload 1911 kg.

Country of origin
The EU
Appointment
passenger
Crew.
1
Passengers
8
Flight dataV max, km/h
306
V Crase., km/h
276
The rate of climb, m/sec
8,9
The flight range, km
827
The flight duration, an hour
4,3
Max. height, m
4575
Power plant

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Number of engines
2
Engine model
Turbomeca Arriel 2C
Engine type
gas turbine
Power system
injection into the chamber
Fuel
kerosene
Power cruising, S. L.
811
Power take-off, HP
863
The max. power, HP
977
Fuel consumption, l/h
990
The fuselage

The number of doors
4
Equipment

Navigational equipment
for day piloting
Dimensions

Fuselage length, m
11,63
The length of the screw, m
13,73
Main rotor diameter, m
11,94
The diameter of the tail rotor, m
1,10
Height, m
4,06
Wheel track, m
2,03
Weight, weight

Full take-off weight, kg
4300
Payload, kg
1911
Gas tank

Fuel tank capacity, l
1135
The extra capacity fuel tank, l
180