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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
C-2 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Kawasaki C-2 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | 3: 2 pilots and 1 loadmaster[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Military transport aircraft[source] |
| National origin | United States[source] | Japan[source] |
| Manufacturer | Air Tractor[source] | Kawasaki Aerospace Company |
43.9 m (144 ft 0 in)[source]
AT-802 · Range
Single source800 mi (1,300 km, 700 nmi)[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]
C-2 · 2 × General Electric CF6 -80C2K1F turbofan engines thrust each
Single source2 × General Electric CF6 -80C2K1F turbofan engines, 265.7 kN (59,740 lbf) thrust each[source]
AT-802 · Wing area
Single source401.0 sq ft (37.25 m 2 )[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.
| Status | Active[source] | In service, in production[source] |
|---|
| Manufactured | 1990–present[source] | 2010–present[source] |
|---|
| First flight | 1990[source] | 26 January 2010[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 32 t limited to + 2.5g ; 36 t limited to + 2.25g ; maximum payload 37.6 t Field Operation System or Truck Crane or 8 463L Pallets or 1 UH-60JA helicopter or 1 Type 16 maneuver combat vehicle wheeled tank destroyer[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] | — |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| Number built | — | 21[source] |
|---|
| Introduction date | — | 30 June 2016[source] |
|---|
| Minimum takeoff distance | — | 500 m (1,641 ft)[source] |
|---|