Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
EMB 110P1A/41 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Embraer EMB 110 Bandeirante |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Turboprop regional airliner[source] |
| National origin | United States[source] | Brazil[source] |
| Manufacturer | Air Tractor[source] | Embraer[source] |
| Status | Active[source] | In limited commercial service, in active military service |
15.1 m (49 ft 6 in)[source]
Empty; AT-802 · Empty weight
Single sourceMaximum take-off; AT-802 · Max takeoff weight
Single source6,505 lb (2,951 kg)[source]
16,000 lb (7,257 kg)[source]
Empty; EMB 110P1A/41 · empty equipped - passengers
Single sourceMaximum take-off; EMB 110P1A/41 · Max takeoff weight
Single sourceAT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[source]
EMB 110P1A/41 · 2 × Pratt & Whitney Canada PT6A-34 turboprop engines (750 shp) each
Single source2 × Pratt & Whitney Canada PT6A-34 turboprop engines, 560 kW (750 shp) 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] | 1968–1990[source] |
|---|
| First flight | 1990[source] | 26 October 1968[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 18 passengers[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: NACA 23016 mod. ; tip: NACA 23012[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | Brazilian Air Force Wiggins Airways Transportes Aereos Guatemaltecos[source] |
|---|
| Number built | — | 503[source] |
|---|
| Introduction date | — | 16 April 1973[source] |
|---|
| Fuel capacity | — | 1,308 kg (2,884 lb) / 1,720 L (450 US gal; 380 imp gal) in four integral wing tanks[source] |
|---|
| Propellers | — | 3-bladed Hartzell HC-B3TN-3C/T10178H-8R, 2.36 m (7 ft 9 in) diameter fully-feathering reversible-pitch constant-speed propellers[source] |
|---|
| Economical cruise speed | — | 341 km/h (212 mph; 184 kn) at 3,050 m (10,000 ft)[source] |
|---|
| Take-off run | — | 807 m (2,648 ft) (FAR23.135 / SFAR 41A)[source] |
|---|
| Landing run | — | 868 m (2,848 ft) at MLW[source] |
|---|