Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
An-140 AI-30 engines · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Antonov An-140 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Turboprop regional airliner[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Antonov Aviakor HESA[source] |
| Status | Active[source] | In service[source] |
| Manufactured |
22.605 m (74 ft 2 in)[source]
Empty; AT-802 · Empty weight
Single sourceMaximum take-off; AT-802 · Max takeoff weight
Single source6,505 lb (2,951 kg)[source]
16,000 lb (7,257 kg)[source]
Empty; An-140 AI-30 engines · Empty weight
Single sourceMaximum take-off; An-140 AI-30 engines · Max takeoff weight
Single sourceAT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1990–present[source] |
1997–2016[source] |
| First flight | 1990[source] | 17 September 1997[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 52 pax / 6,000 kg (13,228 lb) max payload[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Designer | — | Antonov[source] |
|---|
| Primary users | — | Ministry of Defense (Russia) Russian Naval Aviation Motor Sich Airlines Yakutia Airlines[source] |
|---|
| Number built | — | 33[source] |
|---|
| Introduction date | — | 2002[source] |
|---|
| Developed into | — | HESA Simourgh[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] |
|---|
| 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] |
|---|