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AT-802  
Initial Operational Capability (IOC): 2002
Maiden Flight: 1990
Total Production: 300
Also Known As: AT-802A Agricultural, AT-802F Air Tanker and AT-802F Fire Boss
Origin: United States of America
Corporations: Air Tractor* and Fire Boss LLC   (*) lead contractor
Parent System: AT-802
Initial Operational Capability (IOC): 2002
Maiden Flight: 1990
Total Production: 300
Family Members: AT-802U
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Description: The Air Tractor AT-802 is a flexible turboprop-powered fixed-wing aircraft capable of performing a variety of missions in support of civil customers such as agricultural work and firefighting. The AT-802 is considered as the world's largest single engine agricultural turboprop aircraft. The basic model, AT-802, has a two-seat cockpit while the AT-802A has a single seat cockpit. The AT-802F is intended for firefighting and is equipped with a computerized firegate. The same model equipped with Wipaire floats for amphibious operations is referred to as the Fire Boss. The first AT-802 aircraft made its maiden flight in 1990 and entered service with US Department for South American coca crop eradication in 2002. So far, more than 300 airplanes have been sold worldwide.

The twin-seat AT-802F Fire Boss is powered by a single Pratt & Whitney PT6A-67AG turboprop engine developing 1,350-shp of power at 1,700 rpm. The engine drives either a five-blade Hartzell HC-B5MP-3F, M11276NS or M11691NS propeller. Alternatively, the Fire Boss can be powered by a Pratt & Whitney PT6A-67F engine developing 1,600-hp. In its firefighting role the aircraft can drop 88 gallons of foam or 820 gallons of water in just 30 seconds.

AT-802 Specifications

Crew: 2
Number of Engines: 1
Propeller Blades: 5
Area
Wing Area: 401 square foot (37.3 square meter)
Dimensions
Height: 13 foot (156 inch)
Length: 37.5 foot (450 inch)
Propeller Diameter: 10 foot (120 inch)
Wingspan: 59 foot (18.0 meter)
Performance
Max Range: 800 mile (695 nautical mile)
Take Off Run Distance: 2,000 foot (610 meter)
Power
Max Power at TakeOff: 1,350 shp (1,007 kW)
Speed
Climb Rate: 850 fpm (4.34 mps)
Cruise Speed: 221 mph (356 kph)
Stall Speed: 105 mph (91 KIAS)
Volume
Fuel Tank Capacity: 254 galon (965 liter)
Weight
Empty Weight: 7,210 pound (3,270 kilogram)
Max Landing Weight: 16,000 pound (7,258 kilogram)
Max Takeoff Weight: 16,000 pound (7.26 ton)
Useful Load: 8,790 pound (3,987 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)

Operators & Related Equipment


Propulsion Systems
PT6A-67AGx1
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