Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
402C Businessliner · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Cessna 402 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | Two pilots[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Corporate transport and airliner[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Cessna |
36 ft 4 + 1 ⁄ 2 in (11.09 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; 402C Businessliner · Empty weight
Single sourceMaximum take-off; 402C Businessliner · 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]
402C Businessliner · 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines each
Single source2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp (242 kW) each[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[source] |
|---|
| Manufactured | 1990–present[source] | 1966–1985[source] |
|---|
| First flight | 1990[source] | August 26, 1965[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | Six passengers[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | NACA 23018 (root) NACA 23015 (tip)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 68 kn (78 mph, 126 km/h) (flaps down, power off) (CAS)[source] |
|---|
| Primary user | — | Cape Air[source] |
|---|
| Number built | — | 2,000+[source] |
|---|
| Introduction date | — | 1967[source] |
|---|
| Developed from | — | Cessna 411[source] |
|---|
| Developed into | — | Cessna 404 Titan Cessna 414[source] |
|---|
| Fuel capacity | — | 206 US gal (172 imp gal; 780 L) usable fuel[source] |
|---|
| Propellers | — | 3-bladed McCauley 0850334-34 constant speed propeller[source] |
|---|
| Never exceed speed | — | 231 kn (266 mph, 428 km/h) ( CAS )[source] |
|---|
| Takeoff distance to 50 ft (15m) | — | 2,195 ft (669 m)[source] |
|---|
| Landing distance from 50 ft (15m) | — | 2,485 ft (757 m)[source] |
|---|