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]
Citation Latitude · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Cessna Citation Latitude |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Corporate jet[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Textron Aviation[source] |
| Status | Active[source] | In production |
62 ft 3 in (18.97 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; Citation Latitude · Empty weight
Single sourceMaximum take-off; Citation Latitude · 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]
Citation Latitude · 2 × Pratt Whitney Canada PW306D1 turbofan thrust each
Single source2 × Pratt Whitney Canada PW306D1 turbofan, 5,907 lbf (26.28 kN) thrust each[source]
Citation Latitude · Maximum payload
Single source2,544 lb (1,154 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 2014–present[source] |
|---|
| First flight | 1990[source] | 18 February 2014[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] |
|---|
| Aspect ratio | 8.8:1[source] | 9.64[source] |
|---|
| Airfoil | NACA 4415[source] | 16.3° sweep[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Number built | — | 400 by May 2024[source] |
|---|
| Developed from | — | Cessna Citation Sovereign[source] |
|---|
| Developed into | — | Cessna Citation Longitude[source] |
|---|
| Fuel capacity | — | 11,394 lb (5,168 kg)[source] |
|---|
| Cabin | — | 72 in (1.83 m) height × 77 in (1.96 m) width[source] |
|---|
| Never exceed speed | — | 460 kn (530 mph, 850 km/h) Mach .80[source] |
|---|
| Time to altitude | — | 16 min to FL370[source] |
|---|
| Wing loading | — | 56.7 lb/sq ft (277 kg/m 2 ) MTOW[source] |
|---|
| Thrust/weight | — | 0.38[source] |
|---|
| Takeoff | — | 3,580 ft (1,091 m)[source] |
|---|
| Landing | — | 2,480 ft (756 m)[source] |
|---|