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Military


AT-802U

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)
MAIN WHEEL SIZE32.0 in (81.28 cm)
MAXIMUM SPEED, NO WEAPONS,
AT 10,000 FT (3,048 M)		213 knots (394 kph)
PATROLLING SPEED
AT 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 WEIGHT		91 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 RUN1,200 ft (366 m)
Standard Features
  • Ballistic glass and cockpit/engine armor
  • Self-sealing fuel tanks and emergency fuel tank shut-off
  • AMSAFE Inflatable Restraint system integrated with a 5-point harness
  • Air conditioner
  • Large and reconfigurable fuel system
  • Rough strip, off-airfield landing gear
  • High dust environment air induction system
    • Capabilities
  • Rugged and Reliable - The Air Tractor 802U is purpose-built for austere operations
  • Effective and Flexible - Combatproven, multi-mission open systems architecture to “collapse the stack,” replacing multiple aircraft with a single aircraft
  • Persistence and Payload - 6-hour loiter at 200 nm combat radius; 6,000 lb flexible combat load-out
  • Connected - Robust suite of radios and datalinks providing multiple means for line-of-sight (LOS) and beyond line-of-sight (BLOS) communications
  • Situational Awareness - Ability to host multiple EO/IR, ISR and targeting sensors
  • Affordable and Sustainable - Low production and operating costs, backed by an established global sustainment network
  • SOF Heritage - Mature system built on 1.3 million hours of ISR and Strike support and upgrades driven by mission operators
  • Production-Ready - Delivery in less than 12 months

    • GROSS WEIGHTTAKEOFF ROLLRATE 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 fpm (670 mpm)
    SURVEILLANCE & WEAPONS LOAD,
    14,500 LBS (6,600 KG)    		1,400 ft (426 m)1,700 fpm (518 mpm)



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