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]
L-410 UVP-E20 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Let L-410 Turbolet |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Regional airliner , cargo aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Let Kunovice[source] |
| Status | Active[source] | In service[source] |
14.42 m (47 ft 4 in)[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]
L-410 UVP-E20 · 2 × General Electric H80-200 turboprop engines each
Single source2 × General Electric H80-200 turboprop engines, 597 kW (801 hp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1990–present[source] |
1971–present[source] |
| First flight | 1990[source] | 16 April 1969[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Aircraft Industries L 410 NG[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 19 passengers / 1,800 kg (3,968 lb) payload[source] |
|---|
| Aspect ratio | 8.8:1[source] | 11.45[source] |
|---|
| Airfoil | NACA 4415[source] | root: NACA 63A418 ; tip: NACA 63A412[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | Russian Air Force Slovak Air Force Searca Aeroflot (historical)[source] |
|---|
| Number built | — | 1,200[source] |
|---|
| Introduction date | — | 1970[source] |
|---|
| Developed into | — | Let L-610[source] |
|---|
| Fuel capacity | — | 1,300 kg (2,866 lb)[source] |
|---|
| Endurance | — | Five hours and six minutes[source] |
|---|
| Propellers | — | 5-bladed Avia AV 725, 2.3 m (7 ft 7 in) diameter[source] |
|---|
| Fuel consumption | — | 240 kg/h (529 lb/h)[source] |
|---|
| Take-off run | — | 510 m (1,670 ft) (ISA, SL, MTOW)[source] |
|---|
| Landing run | — | 500 m (1,600 ft) (ISA, SL, MTOW)[source] |
|---|
| Alternative designation | — | L-410 Turbolet[source] |
|---|
| Country of origin | — | Czechoslovakia[source] |
|---|