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]
A-50E · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Beriev A-50 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Airborne early warning and control[source] |
| National origin | United States[source] | Soviet Union[source] |
| Manufacturer | Air Tractor[source] | Beriev[source] |
| Status | Active[source] | In service |
46.6 m (152 ft 11 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]
A-50E · 4 × Soloviev D-30KP turbofan engines thrust each
Single source4 × Soloviev D-30KP turbofan engines, 117.68 kN (26,445 lbf) thrust each[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
A-50E · with internal fuel and maximum payload
Single source4 hours with internal fuel and maximum payload[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1978–1992[source] |
|---|
| First flight | 1990[source] | 19 December 1978[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] | — |
|---|
| Airfoil | NACA 4415[source] | root: TsAGI P-151 (13%); tip: TsAGI P-151 (10%)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | Russian Aerospace Forces Indian Air Force[source] |
|---|
| Number built | — | ~42[source] |
|---|
| Introduction date | — | 1985[source] |
|---|
| Developed from | — | Ilyushin Il-76[source] |
|---|
| Developed into | — | Beriev A-100[source] |
|---|
| Guns | — | 2 x 23 mm (0.906 in) GSh-23 autocannons at the base of the rudder[source] |
|---|
Maximum take-off; A-50E · ) based on if the A-50 is based on the Il-76M (
Single sourceMaximum take-off; A-50E · Max takeoff weight
Single sourceMaximum take-off; A-50E · ) or Il-76MD (
Single source