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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
EMB 121A1 Xingu II · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Embraer EMB 121 Xingu |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | 1/2[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Utility aircraft[source] |
| National origin | United States[source] | Brazil[source] |
| Manufacturer | Air Tractor[source] | Embraer |
12.25 m (40 ft 2 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 121A1 Xingu II · equipped
Single sourceMaximum take-off; EMB 121A1 Xingu II · Max takeoff weight
Single sourceCruise; 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]
EMB 121A1 Xingu II · 2 × Pratt & Whitney Canada PT6A-135 turboprop engines each
Single source2 × Pratt & Whitney Canada PT6A-135 turboprop engines, 559 kW (750 hp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | Active[source] |
|---|
| Manufactured | 1990–present[source] | 1977-1987[source] |
|---|
| First flight | 1990[source] | 10 October 1976[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 9 passengers or 770 kg (1,700 lb) cargo with 1 pilot[source] |
|---|
| Aspect ratio | 8.8:1[source] | 7.18[source] |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 141 km/h (87 mph, 76 kn) power off, flaps down[source] |
|---|
| Primary users | — | French Air and Space Force Brazilian Air Force French Navy[source] |
|---|
| Number built | — | 106[source] |
|---|
| Introduction date | — | 20 May 1977[source] |
|---|
| Developed from | — | EMB 110 Bandeirante[source] |
|---|
| Fuel capacity | — | 1,308 kg (2,884 lb)[source] |
|---|
| Propellers | — | 4-bladed Hartzell HC-B4TN-3C/T9212B, 2.36 m (7 ft 9 in) diameter constant-speed metal propeller with auto-feathering and full reverse-pitch[source] |
|---|
| Wing loading | — | 206.2 kg/m 2 (42.2 lb/sq ft)[source] |
|---|
| Fuel consumption | — | 0.52 kg/km (1.86 lb/mi) : 250 lb (110 kg)/h per engine at 234 kn (433 km/h) TAS, FL200, -4°C[source] |
|---|
| Power/mass | — | 0.197 kW/kg (0.12 shp/lb)[source] |
|---|