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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Learjet 36A · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Learjet 35 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | two (pilot and copilot)[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Business jet[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Learjet[source] |
48 ft 8 in (14.83 m)[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]
Learjet 36A · 2 × Garrett TFE731-2-2B turbofans thrust each
Single source2 × Garrett TFE731-2-2B turbofans , 3,500 lbf (16 kN) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status |
|---|
Active[source] |
Operational[source] |
| Manufactured | 1990–present[source] | 1973–1994[source] |
|---|
| First flight | 1990[source] | 22 August 1973[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] | 5.74:1[source] |
|---|
| Airfoil | NACA 4415[source] | NACA 64A-109 (mod)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 96 kn (110 mph, 178 km/h) (wheels and flaps down)[source] |
|---|
| Primary user | — | General aviation, United States Air Force[source] |
|---|
| Number built | — | 738[source] |
|---|
| Developed from | — | Learjet 25[source] |
|---|
| Fuel capacity | — | 1,110 US gal (920 imp gal; 4,200 L) usable fuel[source] |
|---|
| Take-off run to 30 ft (9 m) | — | 4,784 ft (1,458 m)[source] |
|---|
| Landing run from 50 ft (15 m) | — | 2,884 ft (879 m)[source] |
|---|
| Country of origin | — | United States[source] |
|---|