Air Tractor AT-500

Summary

Description

The Air Tractor AT-500 family of agricultural aircraft was first flown on April 25, 1986, in the United States by Air Tractor Inc. The AT-500 is a monoplane with a low-wing and taildragger configuration. It was designed with a chemical hopper situated between the engine firewall and the cockpit. A key feature distinguishing the AT-500 from its predecessors was its increased wingspan of 50 inches (12.7 cm) and a fuselage stretch of 22 inches (56 cm), which allowed for a larger chemical hopper. Almost all variants were designed to accommodate a widened "buddy" seat or a tandem seat for a passenger, observer, or loader, and trainer aircraft with full dual controls were also offered.

The Air Tractor AT-500 family is primarily designed for agricultural applications and is not equipped with traditional military armament. Its main payload is a chemical hopper located between the engine firewall and the cockpit, capable of carrying 500 US gal (420 imp gal; 1,900 L). The aircraft has a substantial payload capacity of 5,830 lb (2,640 kg), allowing it to effectively disperse agricultural chemicals.

As an agricultural aircraft, the Air Tractor AT-500 family has seen extensive operational use in various regions around the globe, wherever aerial application of chemicals and fertilizers is required. Its deployment spans a wide range of agricultural settings, from large-scale farming operations to smaller, more specialized applications. The aircraft's operational strengths include its robust design, high payload capacity, and efficient performance, making it well-suited for demanding agricultural tasks. The AT-502B became the world's top-selling agricultural aircraft between 2011 and 2018, with 388 deliveries.

Main Variants:

• AT-501: The initial piston-powered version featured a 600 shp Pratt & Whitney R-1340 engine, accommodating a single seat, and had a gross weight of 6,500 lb.

• AT-502: An upgraded version of the AT-501, it was equipped with either a 680 shp Pratt & Whitney Canada PT6A-15AG or a 750 shp PT6A-34AG engine, and offered one or two seats with a gross weight of either 6,500 lb or 8,000 lb depending on production date and wing spar type.

• AT-502A: Optimized for high-altitude and high-temperature environments, this variant utilized a more powerful 1,100 shp PT6A-65AG or 1,050 shp PT6A-60AG engine, and provided options for one or two seats in either a tandem or side-by-side arrangement.

• AT-502B: Serving as the primary production model, it evolved from the AT-502, featuring a 750 shp PT6A-34AG engine, and offering one or two seats configured in tandem or side-by-side.

• AT-504: This dual-control trainer variant of the AT-502B was equipped with side-by-side seating, replacing the tandem-seat AT-503 trainers, and was introduced in 2009.

Technical specifications

Current operating countries

Country		Units
	Kenya	0 (+2)

Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.

All operators

Kenya • United States

Photo of AT-500