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]
Thrush Commander 600 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Ayres Thrush |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | one[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Aerial application aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Ayres Corporation Thrush Aircraft |
29 ft 2 in (8.89 m)[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; Thrush Commander 600 · Empty weight
Single sourceMaximum take-off; Thrush Commander 600 · Max takeoff weight
Single sourceCruise; AT-802 · at 8,000 ft (2,440 m)
Single source221 mph (356 km/h, 192 kn) at 8,000 ft (2,440 m)[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]
Thrush Commander 600 · 1 × Pratt & Whitney R-1340 Wasp 9-cylinder air-cooled radial engine
Single source1 × Pratt & Whitney R-1340 Wasp 9-cylinder air-cooled radial engine , 600 hp (450 kW)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | In production[source] |
|---|
| Manufactured | 1990–present[source] | 1956-present[source] |
|---|
| First flight | 1990[source] | 1956[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 400 US gal (330 imp gal; 1,500 L) liquids or 3,280 lb (1,490 kg) dry chemicals[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] | 66 mph (106 km/h, 57 kn) (at 6,000 lb (2,700 kg), flaps down)[source] |
|---|
| Designer | — | Leland Snow[source] |
|---|
| Number built | — | less than 2,000[source] |
|---|
| Fuel capacity | — | 106 US gal (88 imp gal; 400 L)[source] |
|---|
| Propellers | — | 2-bladed Hamilton-Standard 12D40 metal constant speed propeller[source] |
|---|