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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Cessna Citation Ultra · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Cessna Citation V |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Corporate jet[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Cessna[source] |
| Status | Active[source] | — |
48 ft 11 in (14.9 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; Cessna Citation Ultra · BOW
Single sourceMaximum take-off; Cessna Citation Ultra · Max takeoff weight
Single sourceAT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[source]
Cessna Citation Ultra · 2 × Pratt & Whitney Canada JT15D -5D turbofans thrust each
Single source2 × Pratt & Whitney Canada JT15D -5D turbofans , 3,045 lbf (13.54 kN) thrust 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] |
1989 (V) – 2011 (Encore+)[source] |
| First flight | 1990[source] | August 1987[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 7–11 passengers[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 users | — | United States Army United States Marine Corps[source] |
|---|
| Number built | — | 774 : 262 V, 279 Ultra, 168 Encore, 65 Encore+[source] |
|---|
| Introduction date | — | 1987 (Citation V), 1994 (Ultra), 1998 (Encore)[source] |
|---|
| Developed from | — | Cessna Citation S/II[source] |
|---|
| Fuel capacity | — | 5,771 lb (2,618 kg)[source] |
|---|
| Max. Payload | — | 2,275 lb (1,032 kg)[source] |
|---|
| Cabin length | — | 17.4 ft (5.3 m)[source] |
|---|
| Cabin height × width | — | 4.8 ft × 4.9 ft (1.5 × 1.5 m)[source] |
|---|
| Fuel consumption | — | 2.4 lb/mi (0.67 kg/km) at FL410, 433 kn (802 km/h)[source] |
|---|
| Cabin pressurization | — | 8.9 psi (0.61 bar)[source] |
|---|
| Reported operators | — |
|
|---|