Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Jetstream 41 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | British Aerospace Jetstream 41 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Regional airliner /Feederliner[source] |
| National origin | United States[source] | United Kingdom[source] |
| Manufacturer | Air Tractor[source] | British Aerospace[source] |
| Status | Active[source] | In service |
63 ft 2 in (19.25 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]
Jetstream 41 · 2 × Allied Signal TPE331-14GR/HR turboprop engines, 1,650 shp ( ) each (handed GR / HR
Single source2 × Allied Signal TPE331-14GR/HR turboprop engines, 1,650 shp (1,230 kW) each (handed GR / HR)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1992–1997[source] |
|---|
| First flight | 1990[source] | 25 September 1991[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 29 passengers[source] |
|---|
| Aspect ratio | 8.8:1[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 | — | Guna Airlines Proflight Zambia[source] |
|---|
| Number built | — | 100[source] |
|---|
| Introduction date | — | 25 November 1992[source] |
|---|
| Developed from | — | British Aerospace Jetstream 31[source] |
|---|
| Maximum zero-fuel weight | — | 21,400 lb (9,707 kg)[source] |
|---|
| Maximum ramp weight | — | 24,100 lb (10,932 kg)[source] |
|---|
| Maximum landing weight | — | 23,300 lb (10,569 kg)[source] |
|---|
| Fuel capacity | — | 727 imp gal (873 US gal; 3,305 L) / 5,960 lb (2,703 kg) maximum[source] |
|---|
| Propellers | — | 5-bladed McCauley , 9 ft 6 in (2.9 m) diameter (handed GR / HR) constant-speed feathering metal propellers[source] |
|---|
| Never exceed speed | — | 315 kn (362 mph, 583 km/h) CAS sea level to 17,400 ft (5,300 m)[source] |
|---|
| Service ceiling on one engine | — | 15,000 ft (4,600 m)[source] |
|---|
| Wing loading | — | 68.42 lb/sq ft (334.1 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.1375 shp/lb (0.2260 kW/kg)[source] |
|---|
| Take-off run | — | 5,000 ft (1,500 m)[source] |
|---|
| Landing run | — | 4,200 ft (1,300 m)[source] |
|---|