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). It is available in two versions, the four seat ADI Stallion and the six-seat Super Stallion.

Specifications (ADI Super Stallion - 350 hp engine)

Data from Jane's All The World's Aircraft 2003–2004)

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.