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-30 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Antonov An-30 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Aerial cartography , reconnaissance and transport[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Antonov[source] |
| Status | Active[source] | In limited service[source] |
24.26 m (79 ft 7 in)[source]
AT-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-30 · 2 × Ivchenko AI-24T VT turboprop engines (2,803 shp) each equivalent
Single source2 × Ivchenko AI-24T VT turboprop engines, 2,090 kW (2,803 shp) each equivalent[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1990–present[source] |
1971 – 1980[source] |
| First flight | 1990[source] | 21 August 1967[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | — |
|---|
| Aspect ratio | 8.8:1[source] | 11.4:1[source] |
|---|
| Airfoil | NACA 4415[source] | root: TsAGI S-5-18; tip: TsAGI S-3-13[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Designer | — | Beriev[source] |
|---|
| Primary users | — | Russian Air Force Ukrainian Air Force People's Liberation Army Air Force Romanian Air Force[source] |
|---|
| Number built | — | 123[source] |
|---|
| Introduction date | — | July 1968[source] |
|---|
| Developed from | — | Antonov An-24[source] |
|---|
| Fuel capacity | — | 6,200 L (1,600 US gal; 1,400 imp gal)[source] |
|---|
| Propellers | — | 4-bladed constant-speed propellers[source] |
|---|
| Take-off run | — | 710 m (2,329 ft)[source] |
|---|
| Landing run | — | 670 m (2,198 ft)[source] |
|---|
| Country of origin | — | Soviet Union[source] Soviet Union[source] |
|---|