Specifications & Features

From nose to tail, the 802U has what it takes to excel in demanding operating environments.

AT-802U Dimensional Drawings

AT802-U Dimensional Line Drawing Front View AT802-U Dimensional Line Drawing Top View AT802-U Dimensional Line Drawing Side View

AT-802U Specifications

Engine TypePratt & Whitney PT6A-67F
Engine takeoff SHP –uninstalled1,600 @ 40.3° C, 1,700 rpm
Engine maximum continuous shaft horsepower –uninstalled1,600 @ 27.5° C, 1,700 rpm
Propeller118 in (300 cm) diameter, aluminum Hartzell
Propeller ground clearance39 in (0.99 m)
Gross weight –landing & takeoff16,000 lbs (7,257 kg)
Empty weight, with armor, no weapons7,836 lbs (3,703 kg)
Useful load with ballistic armor8,164 lbs (4,000 kg)
Fuel capacity – wings380 US gal (1,438 L)
Auxiliary fuel capacity – fuselage360 US gal (1,363 L)
Wingspan59.2 ft (18.04 m)
Wing area401 ft2 (37.25 m2)

AT-802U Performance

Maximum speed, no weapons, at 10,000 ft. (3048 m)213 knots (394 kph)
Patrolling speed – 10,000 ft.; 71 US gal per hour (3,048 m; 268 L per hour)180 knots (333 kph)
Stall speed – flaps down, at max gross weight91 knots (169 kph)
Stall speed, at 12,500 lbs. (5,670 kg)70 knots (130 kph)
Range with auxiliary fuselage fuel, economy cruise at 8,000 ft (2,438 m)1,303 nm (2,414 km)
Landing run1200 ft (366 m)

AT-802U Performance

Gross Weight Takeoff Roll Rate of Climb
Full fuel load, 10,000 lbs (4,500 kg) 680 ft (207 m) 3,000 fpm (914 mpm)
Surveillance Load, 12,500 lbs (5,700 kg) 1,100 ft (335 m) 2,200 fm (670 mpm)
Surveillance & weapons load, 14,500 lbs (6,600 kg) 1,400 ft (426 m) 1,700 fpm (518 mpm)

AT-802U Standard Features

  • Wing and Center Line Structural External Stores Locations
    • 8 wing hard points to carry 500 lb. class weapons
    • 3 centerline hard points to carry 1,000 lb. class weapons
    • Innermost wing station optimized for guns (.50 cal to 20mm)
  • Pratt & Whitney PT6A-67F Turboprop Engine
  • Titanium Dome 5-Blade Propeller
  • Tandem Seat Cockpit with  Dual Flight Controls, Power and Instruments
  • 380 Gallon Wing Fuel Tanks
  • 360 Gallon Fuselage Fuel Tank, with Fuel Jettison
  • Self-Sealing Fuel System (Wing Tanks, Fuselage Tanks and Fuel Hoses)
  • Fuel Tank Shutoff Control System
  • Cockpit and Engine Armor (Panels, Glass, Split Doors and Footwell enclosure)
  • Vertical Speed Indicator (Front Cockpit)
  • Lightning Protection
  • AmSafe Inflatable Restraints, (Front and Rear Cockpit)
  • Minimum VFR Flight Instruments
  • ESC Electrical Bus
  • Forward Mission Equipment Bay
  • NVG Compatible Cockpit Lighting
  • Emergency Locator Transmitter (ELT)
  • Two-Place Diluter Extended Demand Oxygen System
  • Avionics (Air Speed Indicator, Turn Coordinator, Altimeter, Altitude Indicator, Clock)