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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
DA62 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Diamond DA62 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | one[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Twin engine light aircraft[source] |
| National origin | United States[source] | Austria[source] |
| Manufacturer | Air Tractor[source] | Diamond Aircraft Industries Aeromot |
9.19 m (30 ft 2 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]
Cruise; DA62 · (TAS) at 75% power
Single sourceMaximum; DA62 · True Air Speed (TAS) at Maximum Continuous Power (MCP) at 14,000 ft (4,267 m)
Single source356 km/h (221 mph, 192 kn) True Air Speed (TAS) at Maximum Continuous Power (MCP) at 14,000 ft (4,267 m).[source]
317 km/h (197 mph, 171 kn) (TAS) at 75% power[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]
DA62 · 2 × Austro AE330 turbocharged 2.0 liter diesel aircraft engines each
Single source2 × Austro AE330 turbocharged 2.0 liter diesel aircraft engines , 134 kW (180 hp) each[source]
DA62 · Endurance
Single source10 h[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | In production (DA62)[source] |
|---|
| Manufactured | 1990–present[source] | 2015–present[source] |
|---|
| First flight | 1990[source] | 3 April 2012[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | up to six 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] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| Number built | — | 273 (April 2024)[source] |
|---|
| Introduction date | — | October 2015[source] |
|---|
| Developed from | — | Diamond DA50[source] |
|---|
| Fuel capacity | — | 326 litres (72 imp gal; 86 US gal)[source] |
|---|
| Propellers | — | 3-bladed MT propeller MTV-6-R-C-F/CF 194-80[source] |
|---|
| Never exceed speed | — | 379 km/h (235 mph, 205 kn)[source] |
|---|
| Fuel consumption | — | 7.4 US gal (28 L) per hour total at loiter, 11.8 US gal (45 L) per hour at 60% (12,000 ft) in total[source] |
|---|