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 · Length
Single source22.605 m (74 ft 2 in)[source]
SR20-G3 · Length
Configuration
| Specification | Antonov An-140 | Cirrus SR20 |
|---|---|---|
| Type | Turboprop regional airliner[source] | Light aircraft[source] |
| Manufacturer | Antonov Aviakor HESA[source] | Cirrus Aircraft[source] |
| Designer | Antonov[source] | — |
| Status | In service[source] | — |
| Primary users | Ministry of Defense (Russia) Russian Naval Aviation Motor Sich Airlines Yakutia Airlines[source] |
26 ft 0 in (7.92 m)[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; SR20-G3 · Empty weight
Single sourceGross; SR20-G3 · Gross weight
Single sourceAn-140 AI-30 engines · with 6,000 kg (13,228 lb) payload at econ. cruise
Single source900 km (560 mi, 490 nmi) with 6,000 kg (13,228 lb) payload at econ. cruise[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]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
An-140 AI-30 engines · Wing area
Single source51 m 2 (550 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 33[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1997–2016[source] | 1999–present[source] |
|---|
| Introduction date | 2002[source] | — |
|---|
| First flight | 17 September 1997[source] | 21 March 1995[source] |
|---|
| Developed into | HESA Simourgh[source] | Cirrus SR22[source] |
|---|
| Capacity | 52 pax / 6,000 kg (13,228 lb) max payload[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 4,370 kg (9,634 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] | 3-bladed[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] | — |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| National origin | — | United States[source] |
|---|