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]
Premier IA · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Beechcraft Premier I |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Business Jet[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Raytheon / Hawker Beechcraft[source] |
| Status | Active[source] | Active[source] |
46 ft 0 in (14.02 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]
Premier IA · 2 × Williams FJ44 -2A Turbofan thrust each
Single source2 × Williams FJ44 -2A Turbofan, 2,300 lbf (10.23 kN) thrust each[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Premier IA · Maximum payload
Single source1,400 lb / 635 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] |
2001-2012[source] |
| First flight | 1990[source] | December 22, 1998[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 6 / 7[source] |
|---|
| Aspect ratio | 8.8:1[source] | 8.03[source] |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Number built | — | 292[source] |
|---|
| Fuel capacity | — | 3,670 lb / 1,665 kg[source] |
|---|
| Cabin Length × Width × Height | — | 13 ft 6 in × 5 ft 6 in × 5 ft 5 in (4.11 × 1.68 × 1.65 m)[source] |
|---|
| Hold | — | 76.9 cu. ft / 2.2 cu. m[source] |
|---|
| Wing loading | — | 50.6 lb/sq ft (247 kg/m 2 )[source] |
|---|
| Fuel consumption | — | 1.67 lb/mi (0.47 kg/km)[source] |
|---|
| Thrust/weight | — | 0.37[source] |
|---|
| Take-off (MTOW) | — | 3,792 ft / 1,156 m[source] |
|---|
| Landing (MLW) | — | 3,177 ft / 968 m[source] |
|---|
| Country of origin | — | United States[source]Beechcraft Premier I · literal inventory Origin field assigned to the exact equipment row linked in the primary inventory identity column; no operator, manufacturer location or parent/sibling specification inference |
|---|