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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Boeing C-32 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | VIP transport, special operations[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Boeing[source] |
| Status | Active[source] | In service |
155 ft 3 in (47.32 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]
2 × Pratt & Whitney PW2000 -40 turbofan engines thrust each
Single source2 × Pratt & Whitney PW2000 -40 turbofan engines, 40,100 lbf (178 kN) thrust each[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] | — |
|---|
| First flight | 1990[source] | — |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 45[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 | — | United States Air Force[source] |
|---|
| Number built | — | C-32A: 8 (4 acknowledged) C-32B: 2[source] |
|---|
| Introduction date | — | June 1998[source] |
|---|
| Developed from | — | Boeing 757[source] |
|---|
| Fuel capacity | — | 13,334 US gal (11,103 imp gal; 50,475 L) with auxiliary tanks in fwd and aft cargo holds[source] |
|---|
| Maximum zero-fuel weight | — | 186,000 lb (84,368 kg) MZFW[source] |
|---|
| Maximum landing weight | — | 210,000 lb (95,254 kg) MLW[source] |
|---|
| Approach speed | — | 137 kn (158 mph; 254 km/h)[source] |
|---|
| Initial cruising height | — | 35,400 ft (10,790 m)[source] |
|---|
| Wing loading | — | 127.88 lb/sq ft (624.4 kg/m 2 )[source] |
|---|
| Thrust/weight | — | 0.314[source] |
|---|
| Take-off field length | — | 7,800 ft (2,377 m) at sea level 29 °C (84 °F)[source] |
|---|
| Landing field length | — | 5,100 ft (1,554 m) at MLW[source] |
|---|
256,000 lb (116,120 kg) MTOW[source]