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]
Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Gulfstream G550 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Business jet[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Gulfstream Aerospace[source] |
| Status | Active[source] | In service |
96 ft 5 in (29.39 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]
2 × Rolls-Royce BR710 C4-11 turbofan engines thrust each
Single source2 × Rolls-Royce BR710 C4-11 turbofan engines, 15,385 lbf (68.44 kN) thrust each[source]
AT-802 · Wing area
Single source401.0 sq ft (37.25 m 2 )[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 2003–2021[source] |
|---|
| First flight | 1990[source] | 31 August 2001[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | L3Harris EA-37B Compass Call[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 14–19 passengers / 6,200 lb (2,812 kg) payload[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: NACA 0012; tip: NACA 0012[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | United States Air Force United States Navy Israeli Air Force[source] |
|---|
| Number built | — | >600[source] |
|---|
| Introduction date | — | 2004[source] |
|---|
| Developed from | — | Gulfstream V[source] |
|---|
| Successors | — | Gulfstream G600[source] |
|---|
| Fuel capacity | — | 41,300 lb (18,733 kg)[source] |
|---|
| Cabin dimensions: height × width × length | — | 6 ft 2 in × 7 ft 4 in × 43 ft 11 in (1.88 m × 2.24 m × 13.39 m); total length including baggage hold: 50 ft 1 in (15.27 m)[source] |
|---|
| Cabin volume | — | 1,669 cu ft (47.26 m 3 ); usable baggage compartment volume: 170 cu ft (4.81 m 3 )[source] |
|---|
| Cabin altitude | — | 6,000 ft (1,829 m)[source] |
|---|
| Maximum landing weight | — | 75,300 lb (34,156 kg)[source] |
|---|
| High Speed Cruise | — | M0.85 at 41,000 ft (12,000 m)[source] |
|---|
| Long Range Cruise | — | M0.80 at 41,000 ft (12,000 m)[source] |
|---|
| Maximum Mach Operating (MMO) | — | M0.885 at 41,000 ft (12,000 m)[source] |
|---|
| Take-off run | — | 5,910 ft (1,800 m)[source] |
|---|
| Landing run | — | 2,770 ft (840 m)[source] |
|---|
Maximum take-off; Max takeoff weight