Air Tractor AT-302

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

142
KTAS
Cruise Speed
1
Occupants
470
nm
Max Range
2756
lbs
Wet Payload

Estimated Ownership Costs

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About the Air Tractor AT-302

Overview

The Air Tractor AT-302, introduced in 1977, holds a historical distinction as Air Tractor’s first turbine-powered agricultural aircraft. While the AT-300 series began with radial engines, the 302 swapped the piston for a Lycoming LTP101 (and later variants used the PT6A) turboprop. This modification provided the reliability and instant power response required for the demanding low-level, high-cycle environment of aerial application. For a GA buyer or specialized operator, it represents an entry-point into turbine utility aviation, though its purpose-built design limits its versatility outside of agriculture or firefighting.

Key Features for GA Buyers

  • Turbine Reliability: The move away from radial engines significantly reduced maintenance downtime and eliminated the complexities of large-displacement piston cooling and vibration.
  • STOL Capability: Designed for operation from short, unimproved farm strips, the AT-302 boasts impressive takeoff performance even when heavily loaded.
  • Hopper Utility: Features a 320 to 385-gallon hopper (depending on sub-variant), designed for rapid loading and precise dispersal of liquid or dry materials.
  • Visibility: The high-seating position and sloped nose provide the pilot with an exceptional view of the working area and obstacles during low-level maneuvers.

Trade-offs

  • Single-Purpose Cockpit: This is a true single-seat workhorse. There is no room for passengers or significant cross-country baggage, making it unsuitable for traditional GA travel.
  • Specific Engine Support: The original LTP101 engine, while innovative, has a smaller support base compared to the ubiquitous Pratt & Whitney PT6A found in later models like the AT-402.
  • High Maintenance Environment: Due to the nature of crop-dusting (constant turns, heavy loads, and chemical exposure), these airframes require rigorous and frequent inspections for corrosion and fatigue.

Technical Specifications

Dimensions

Wingspan
45.1 ft
Length
27.0 ft
Height
8.5 ft

Weights

Max Takeoff Weight
7,400 lbs
Max Landing Weight
7,000 lbs
Useful Load
3,600 lbs
Fuel Capacity
126 gal

Performance

Cruise Speed
142 KTAS
Range
470 NM
Service Ceiling
15,000 ft
Rate of Climb
1600 fpm

Engines

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