Air Tractor AT-302

Turboprop • single engine • Low Wing • Conventional 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

Endorsements & ratings:
  • High-Performance
  • Tailwheel
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
Parking area (ft2)
1763.2 ft2

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
Never-Exceed (Vne)
174 KIAS
Max Structural Cruise (Vno)
142 KIAS
Approach Speed
82 KIAS
Stall, Clean (Vs1)
62 KIAS
Range
470 NM
Service Ceiling
15,000 ft
Rate of Climb
1600 fpm
Takeoff over 50 ft obstacle
1,900 ft
Landing ground roll
820 ft

Engine

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Similar to the Air Tractor AT-302

Air Tractor AT-402 silhouette

Air Tractor AT-402

Cruise
124 kts (lower than this aircraft)
Range
550 nm (higher than this aircraft)
Seats
1
Turboprop single engine Low Wing
Compare
Air Tractor AT-602 silhouette

Air Tractor AT-602

Cruise
158 kts (higher than this aircraft)
Range
520 nm (higher than this aircraft)
Seats
1
Turboprop single engine Low Wing
Compare

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