Air Tractor AT-802

Turboprop • single engine • Low Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

166
KTAS
Cruise Speed
2
Occupants
700
nm
Max Range
7547
lbs
Wet Payload

Estimated Ownership Costs

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About the Air Tractor AT-802

Overview

The Air Tractor AT-802 is the world’s largest single-engine agricultural aircraft and a dominant force in aerial firefighting. Introduced in 1992, it represents the pinnacle of the Air Tractor line, featuring a massive 800-gallon hopper and the robust Pratt & Whitney PT6A-67AG turboprop engine. While the ‘A’ model is a single-seat workhorse, the standard 802 features a tandem two-seat cockpit, making it versatile for training, observation, or specialized government missions. Its reliability and high-payload capacity have even led to its adoption by military forces (as the AT-802U Sky Warden) for light attack and ISR missions.

Key Features for GA Buyers/Operators

  • Unmatched Capacity: With a 16,000 lb MTOW and an 800-gallon hopper, it can perform the work of multiple smaller aircraft in a single sortie.
  • Firefighting Versatility: The AT-802F variant is the industry standard for Single Engine Air Tankers (SEAT), often equipped with the computerized Gen II/III fire gate for precision drops.
  • Amphibious Options: The “Fire Boss” variant adds Wipaire Wipline 10000 floats, allowing the aircraft to scoop water from lakes or rivers while in motion.
  • Extreme Durability: Designed for the high-cycle, high-stress environment of low-level application, featuring a crashworthy cockpit structure and reinforced airframe.

Trade-offs

  • Massive Operating Costs: Between the PT6A-67 engine’s fuel burn (approx. 70-80 GPH) and the specialized maintenance requirements of a 16,000 lb airframe, this is a high-overhead machine.
  • Operational Complexity: Handling 16,000 lbs on a single engine requires significant pilot skill, particularly in the low-and-slow environment where these aircraft live.
  • Restricted Use: Certified in the Restricted Category; while it is the “king of the hill” for utility, it cannot be used for standard civilian passenger transport.

Technical Specifications

Dimensions

Wingspan
59.2 ft
Length
35.9 ft
Height
12.8 ft

Weights

Max Takeoff Weight
16,000 lbs
Max Landing Weight
16,000 lbs
Useful Load
9,249 lbs
Fuel Capacity
254 gal

Performance

Cruise Speed
166 KTAS
Range
700 NM
Service Ceiling
13,000 ft
Rate of Climb
850 fpm

Engines

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