ADI Stallion

Stallion
Role	Light utility aircraft
National origin	United States of America
Manufacturer	Aircraft Designs Inc
Designer	Martin Hollmann
First flight	July 1994

The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding. It is a single-engined high-winged monoplane, with wings based on htose of the Lancair IV and a retractable tricycle landing gear. It has a steel-tube fuselage centre section, with the remainder of the airframe of composite construction, and is designed to be powered by engines of 230–350 hp (172–261 kW).^[1] It is available in two versions, the four seat ADI Stallion and the six-seat Super Stallion.^[2]

Specifications (ADI Super Stallion - 350 hp engine)

Data from Jane's All The World's Aircraft 2003–2004)^[1]

General characteristics

• Crew: one pilot
• Capacity: 5 passengers
• Length: 25 ft 0 in (7.62 m)
• Wingspan: 35 ft 0 in (10.67 m)
• Height: 9 ft 6 in (2.90 m)
• Wing area: 140.1 sq ft (13.00 m²)
• Aspect ratio: 8.8:1
• Empty weight: 2,200 lb (998 kg)
• Max takeoff weight: 3,800 lb (1,784 kg)
• Powerplant: 1 × Continental TSIO-550-B air-cooled turbocharged flat-six engine, 350 hp (224 kW)

Performance

• Maximum speed: 306 mph (266 knots, 493 km/h)
• Cruise speed: 295 mph (256 knots, 474 km/h)
• Stall speed: 71 mph (62 knots, 115 km/h)
• Range: 2,700 miles (2,346 nmi, 4,345 km)
• Service ceiling: 32,000 ft (9,750 m)
• Rate of climb: 2,600 ft/min (13.2 m/s)

See also

Related development

• Lancair IV
  

References

• Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.
• Taylor, Michael. Brassey's World Aircraft & Systems Directory 1999/2000. London: Brasseys, 1999. ISBN 1-85753-245-7.

Aircraft produced by Aircraft Designs Inc Condor • Stallion • Sportster • Bumble Bee

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