Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
330-200 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Short 330 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | Three (two pilots plus one cabin crew )[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Transport aircraft[source] |
| National origin | United States[source] | United Kingdom[source] |
| Manufacturer | Air Tractor[source] | Short Brothers |
17.69 m (58 ft 0 in)[source]
Cruise; 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]
330-200 · 2 × Pratt & Whitney Canada PT6 A-45-R turboprop (1,198 shp) each
Single source2 × Pratt & Whitney Canada PT6 A-45-R turboprop , 893 kW (1,198 shp) 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 limited cargo service[source] |
|---|
| Manufactured | 1990–present[source] | 1974–1992[source] |
|---|
| First flight | 1990[source] | 22 August 1974[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | C-23A Sherpa[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | — |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | NACA 63A series (modified)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 135 km/h (84 mph, 73 kn) (landing gear and flaps down)[source] |
|---|
| Primary users | — | Air Cargo Carriers Corporate Air[source] |
|---|
| Number built | — | 330-100: 68 330-200: 73[source] |
|---|
| Introduction date | — | 1976[source] |
|---|
| Developed from | — | Short Skyvan[source] |
|---|
| Developed into | — | Short 360[source] |
|---|
| Fuel capacity | — | 2,546 L (560 imp gal; 673 US gal)[source] |
|---|
| Propellers | — | 5-bladed Hartzell constant-speed[source] |
|---|