| Class | Helicopter |
| Max. passengers | 9 |
| Year of production |
2019
PRO
|
| Serial number | 20291 |
| Homebase | LGAV (ATH), Eleftherios Venizelos Intl |
| Cabin height | 1.26 m |
| Cabin width | 1.50 m |
| Cabin length | 1.87 m |
| Luggage volume | 1.00 m³ |
| Last seen | LGAV, Eleftherios Venizelos Intl |
Airbus H145 is the result of constant reinvention.
Designed to deliver excellent performance throughout the flight envelope, Airbus’ H145 is the latest member of its 4-ton-class twin-engine rotorcraft product range – with designed-in mission capability and flexibility, especially in high and hot operating conditions.
The H145 offers exceptional performance thanks to Safran Helicopter engines Arriel 2E power plant and dual full-authority digital engine control (FADEC) – along with the helicopter’s upgraded main and tail rotor systems. This guarantees an unprecedented level of performance.
Equipped with the latest Airbus’ Helionix avionics system which is designed for greater mission flexibility and operational safety.
The Fenestron technology brings benefits such as improved flight and ground safety to customers, as well as enhanced anti-torque control efficiency, reduced power demand in forward flight, and lower sound and vibration levels.
Designed to deliver excellent performance throughout the flight envelope, Airbus’ H145 is the latest member of its 4-ton-class twin-engine rotorcraft product range – with designed-in mission capability and flexibility, especially in high and hot operating conditions.
The H145 offers exceptional performance thanks to Safran Helicopter engines Arriel 2E power plant and dual full-authority digital engine control (FADEC) – along with the helicopter’s upgraded main and tail rotor systems. This guarantees an unprecedented level of performance.
Equipped with the latest Airbus’ Helionix avionics system which is designed for greater mission flexibility and operational safety.
The Fenestron technology brings benefits such as improved flight and ground safety to customers, as well as enhanced anti-torque control efficiency, reduced power demand in forward flight, and lower sound and vibration levels.
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