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At a glance
Measured figures
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; EA-18G Growler · Empty weight
Single sourceGross; EA-18G Growler · recovery weight
Single sourceMaximum take-off; EA-18G Growler · Max takeoff weight
Single sourceMaximum take-off; Official specification · ; 66,000 pounds (29,937 kilograms)
Manufacturer claim33,094 lb (15,011 kg)[source]
48,000 lb (21,772 kg) ; recovery weight[source]
66,000 lb (29,964 kg)[source]
66,000 pounds (29,937 kilograms)[source]
AT-802 · Range
Single source800 mi (1,300 km, 700 nmi)[source]
EA-18G Growler · for interdiction mission
Single source390 nmi (449 mi, 722 km) ; for interdiction mission[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]
EA-18G Growler · 2 × General Electric F414-GE-400 turbofans thrust each dry
Single sourceEA-18G Growler · with afterburner
Single source2 × General Electric F414-GE-400 turbofans , 14,000 lbf (62 kN) thrust each dry, 22,000 lbf (98 kN) with afterburner[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.
Configuration
| Specification | Air Tractor AT-802 | Boeing EA-18G Growler |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Carrier-based electronic-warfare aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Boeing[source] |
| Status | Active[source] | In service[source] |
| Manufactured | 1990–present[source] | 2004–2019[source] |
| First flight | 1990[source] | 15 August 2006[source] |
| Variant | L3Harris OA-1K Skyraider II[source] | — |
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | — |
| Aspect ratio | 8.8:1[source] | — |
| Airfoil | NACA 4415[source] | — |
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
| Primary users | — | United States Navy Royal Australian Air Force[source] |
| Number built | — | 172 as of October 2021[source] |
| Introduction date | — | 22 September 2009[source] |
| Developed from | — | Boeing F/A-18F Super Hornet[source] |
| Guns | — | None[source] |
| Hardpoints | — | 9 total: 6 under-wing and 3 under-fuselage with a capacity of 17,750 lb (8,050 kg) external fuel and ordnance[source] |
| Internal fuel capacity | — | 13,940 lb (6,323 kg)[source] |
| External fuel capacity | — | (3 x 480 gal (1,800 L) tanks), 9,774 lb (4,420 kg)[source] |
| Wing loading | — | 92.8 lb/sq ft (453 kg/m 2 )[source] |
| Thrust/weight | — | 0.93[source] |
| Notes | — | The two wingtip missile launcher rails for AIM-9 Sidewinder , found on the E/F Super Hornet, have been replaced with AN/ALQ-218 detection pods, six removable under wing mounted hard points (inboard pylons will carry 480 gal (1,800 L) fuel tanks, mid-board pylons will carry AN/ALQ-99 High Band Jamming Pods, and outboard pylon reserved for AGM-88 HARM missiles), two multi-mode conformal fuselage stations ( AIM-120 AMRAAM missiles), 1 centerline fuselage removable hardpoint, for AN/ALQ-99 Low Band Jamming Pod.[source] |