There are 3 images added on 28 June 2011
Initial Operational Capability (IOC): 2011
Maiden Flight: 2009
Total Production: ?
Origin: United States of America
Corporations: Air Tractor* and Combined Air Ventures   (*) lead contractor
Parent System: AT-802
Initial Operational Capability (IOC): 2002
Maiden Flight: 1990
Total Production: 300
Family Members: AT-802
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Description: The Air Tractor AT-802U is a twin-seat version indented to provide a 10-hour Intelligence, Surveillance and Reconnaissance (ISR) capability while carrying a 8,000-lb of payload including sensors, bombs, missiles, rockets and machine guns. The aircraft can load a variety of EO/IR (Electro-Optical/Infrared), SIGINT (Signals Intelligence) or SAR (Synthetic Aperture Radar) payload. An optional retractable L3 Wescam MX-15Di sensor targeting pod and ROVER video downlink lets ground commanders, other aircraft and forward air controllers see the battle space in real time. The AT-802U carried out successfully its maiden flight in 2009 and has been optimized for operations from unprepared and unpaved runways.

The AT-802U features 11 hard points on the wings and fuselage that can accept two GAU-19/A 12.7mm machine guns, 8 Hellfire missiles, 500-lb and/or 250-lb laser guided bombs, 16 DAGR rockets and up to six mini Talon weapons. For enhanced combat survivability the cockpit and engine have been placed inside an armored box. Fuel tanks and lines are self-sealing. Ballistic glass windshields and side windows have defeated bullets during counterdrug operations. The AT-802U airplane is powered by a single Pratt & Whitney PT6A-67F turboprop engine developing 1,600-hp of power.

AT-802U Specifications

Crew: 2
External Stations: 11
Number of Engines: 1
Propeller Blades: 5
Wing Area: 401 square foot (37.3 square meter)
Main Gun Caliber: 12.7 millimeter
Propeller Diameter: 118 inch
Wingspan: 59 foot (18.0 meter)
Ceiling: 10,000 foot (3,048 meter)
Landing Run Distance: 1,200 foot (366 meter)
Max Range: 1,303 nautical mile (2,413 kilometer)
Max Power at TakeOff: 1,600 shp
Cruise Speed: 180 knot (333 kph)
Stall Speed: 70 knot (130 kph)
Top Speed at High Altitude: 213 knot (394 kph)
Fuel Tank Capacity: 380 galon (1,444 liter)
Empty Weight: 7,836 pound (3.55 ton)
Max Landing Weight: 16,000 pound (7,258 kilogram)
Max Takeoff Weight: 16,000 pound (7.26 ton)
Useful Load: 8,164 pound (3,703 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

AT-802U News

There is 1 news
on 23 Jan 2017
Monday, January 23, 2017FMS: Kenya Seeks 12 Air Tractor Aircraft with Weapons and Related Support

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