Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
B55 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Beechcraft Baron |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Civil utility aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Beechcraft[source] |
| Status | Active[source] | In production |
28 ft 0 in (8.53 m)[source]
Cruise; 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]
B55 · 2 × Continental IO-470-L air-cooled six-cylinder horizontally opposed engines each
Single source2 × Continental IO-470-L air-cooled six-cylinder horizontally opposed engines, 260 hp (190 kW) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1961–present[source] |
|---|
| First flight | 1990[source] | February 29, 1960[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 6 passengers[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | NACA 23016.5 at root, NACA 23010.5 at tip[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 73 kn (84 mph, 135 km/h) IAS , power off, wheels and flaps lowered[source] |
|---|
| Primary user | — | United States Army (historical)[source] |
|---|
| Number built | — | 7,011 (at end of 2025)[source] |
|---|
| Developed from | — | Beechcraft Travel Air[source] |
|---|
| Fuel capacity | — | 100 US gal (83 imp gal; 380 L) usable fuel (normal), 136 US gal (113 imp gal; 510 L) with optional tanks[source] |
|---|
| Takeoff distance to 50 ft (15m) | — | 1,675 ft (511 m)[source] |
|---|
| Landing distance from 50 ft (15m) | — | 1,840 ft (560 m)[source] |
|---|