Credit
Dmitry A. Mottl · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-140 AI-30 engines · Height
Single source8.225 m (27 ft 0 in)[source]
Empty; An-140 AI-30 engines · Empty weight
Single sourceMaximum take-off; An-140 AI-30 engines · Max takeoff weight
Single source12,810 kg (28,241 lb)[source]
19,150 kg (42,219 lb)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceCruise; An-140 AI-30 engines · at 7,200–7,500 m (23,600–24,600 ft) max
Single source575 km/h (357 mph, 310 kn) at 7,200–7,500 m (23,600–24,600 ft) max[source]
An-140 AI-30 engines · 2 × Motor-Sich AI-30 series 1 turboprop engines each (licence-built Klimov TV3-117VMA-SBM1 )
Single source2 × Motor-Sich AI-30 series 1 turboprop engines, 1,838 kW (2,465 hp) each (licence-built Klimov TV3-117VMA-SBM1 )[source]
Falcon 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each[source]
An-140 AI-30 engines · 1,344 ft/min
Single source6.83 m/s (1,344 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Antonov An-140 | Dassault Falcon 900 |
|---|---|---|
| Type | Turboprop regional airliner[source] | Business jet[source] |
| Manufacturer | Antonov Aviakor HESA[source] | Dassault Aviation[source] |
| Designer | Antonov[source] | — |
| Status | In service[source] | Active service, in production[source] |
| Primary users | Ministry of Defense (Russia) Russian Naval Aviation Motor Sich Airlines Yakutia Airlines[source] | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
| Number built | 33[source] | >500[source] |
| Manufactured | 1997–2016[source] | 1984–present[source] |
| Introduction date | 2002[source] | — |
| First flight | 17 September 1997[source] | 21 September 1984 ( 1984-09-21 )[source] |
| Developed into | HESA Simourgh[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
| Capacity | 52 pax / 6,000 kg (13,228 lb) max payload[source] | 19 passengers[source] |
| Fuel capacity | 4,370 kg (9,634 lb)[source] | 8,690 kg (19,160 lb)[source] |
| Maximum zero fuel weight | 17,800 kg (39,242 lb)[source] | — |
| Maximum landing weight | 19,100 kg (42,108 lb)[source] | — |
| Alternate engines | 2x Pratt & Whitney Canada PW127A turboprops driving Hamilton Sundstrand 247F propellers[source] | — |
| Propellers | 6-bladed Aerosila SV-14, 3.6 m (11 ft 10 in) diameter constant-speed fully feathering reversible propellers[source] | — |
| Economical cruise speed | 520 km/h (320 mph; 280 kn) at 7,200–7,500 m (23,600–24,600 ft)[source] | — |
| Power/mass | 0.19 kW/kg (0.12 hp/lb)[source] | — |
| Balanced field length | 1,350 m (4,429 ft)[source] | — |
| Country of origin | Ukraine[source] | — |
| National origin | — | France[source] |
| Developed from | — | Dassault Falcon 50[source] |
| Aspect ratio | — | 7.63:1[source] |
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |