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]
T210N Turbo Centurion II · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Cessna 210 Centurion |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | One[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Cessna |
28 ft 2 in (8.59 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; T210N Turbo Centurion II · Empty weight
Single sourceGross; T210N Turbo Centurion II · Gross 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]
T210N Turbo Centurion II · 1 × Continental Motors TSIO-520-R air-cooled turbocharged flat-six
Single source1 × Continental Motors TSIO-520-R air-cooled turbocharged flat-six , 310 hp (230 kW)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | — |
|---|
| Manufactured | 1990–present[source] | 1957–1986[source] |
|---|
| First flight | 1990[source] | January 1957[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | Five 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] | 58 kn (67 mph, 107 km/h) (power off, flaps down) ( CAS )[source] |
|---|
| Number built | — | 9,240[source] |
|---|
| Introduction date | — | 1957[source] |
|---|
| Developed from | — | Cessna 182 Skylane[source] |
|---|
| Developed into | — | Cessna 205/206/207[source] |
|---|
| Fuel capacity | — | 87 US gal (72 imp gal; 330 L) (usable capacity)[source] |
|---|
| Propellers | — | 3-bladed McCauley Type D3A34C402/90DFA-10 constant-speed propeller , 7 ft 6 in (2.29 m) diameter[source] |
|---|
| Takeoff distance to 50 ft (15 m) | — | 2,160 ft (660 m)[source] |
|---|
| Landing distance from 50 ft (15 m) | — | 1,500 ft (460 m)[source] |
|---|
| Alternative designation | — | Cessna 210[source] |
|---|