Performance specification

  Performance specification


Passenger capacity
Maximum takeoff weight
Maximum landing weight
Maximum payload

52 persons
21500 kg
21000 kg
6000 kg

    gravity filling
    single point fueling
Maximum cruising speed

4440 kg
4440 kg
537 km/h


  AN-140 aircraft in three views



AN-140 aircraft – side viewAN-140 aircraft – view from above
AN-140 aircraft – front view


Navigation Equipment


- Shoran Âååð-Ì
- VOR/ILS system Êóðñ-93Ì
- RMI ÐÌÈ-3
- Weather radar Áóðàí À-140
- DME ÂÍÄ-94
- Satellite navigation system ÑÍ-3301 (NAVSTAR/GLONASS)
- Radio altimeter À-037
- Transponder ÑÎ-72Ì
- Automatic control system ÑÀÓ-8-02
- Compass system ÁÑÔÊ-1
- Gyro unit ÃÀ-8
- Magnetic compass ÊÈ-13ÁÑ
- Erecting cut-out switch ÂÊ-90Ì
- Flight level alerting system ÑÑÂÝ-ÌÏÁ-Ì
- Flight environment data system ÑÎÑ-140
- Ground proximity warning system ÑÏÏÇ-1-2

   Radiocommunication Equipment

- Radio station Îðëàí-85 ÑÒÀ (ÌÂ) - 2 sets
- Intercom Ëàéíåð-ÌÂË
- Voice recorder Îïàë-Á
- Audio recorder Ìîðèîí-ÁÊ
- Headset ÃÑØ-À-18 - 3 sets
- Emergency radio station Ð-855À1 (VHF/UHF)
- Emergency rescue radio station Ð-861 (SW)
- Emergency transmitter ÊÎÑÏÀÑ ÀÐÁ-ÏÊ-10


Two turboprop engines ÒÂ3-117ÂÌÀ-ÑÁÌ1

designed by Progress Design Bureau sited in Zaporozhye, Ukraine, and manufactured by Motor Sich 

 

Takeoff mode at:
Ðn=101,3 kPa (760 mm of mercury), Ìn=0, tn=+30 Ñ
- kW (horse-power) 1838 (2500)
Full throttle at:
Ðn=101,3 kPa (760 mm of mercury), Ìn=0, tn=+30 Ñ
- kW (horse-power) 2059 (2800)
Maximum cruising mode at:
Í=6000 ì, Ìn=0,5 SÀ
- kW (horse-power) 1286 (1750)

 Load-range diagram
Payload, t



Flying range, km