ADI Stallion

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The ADI Stallion is a US civil utility aircraft that first flew in 1994. It is marketed in kit form for home-building. Large for a homebuilt aircraft, it can seat six people and features retractable tricycle undercarriage.

[edit] Specifications (ADI Stallion)

[edit] General characteristics

  • Crew: one pilot
  • Capacity: 5 passengers
  • Length: 25 ft 0 in (7.62 m)
  • Wing span: 35 ft 0 in (10.67 m)
  • Height: 9 ft 6 in (2.90 m)
  • Wing area: ft² (39 m²)
  • Empty: 2,200 lb (1,000 kg)
  • Loaded: lb ( kg)
  • Maximum takeoff: lb ( kg)
  • Powerplant: 1x TCM IO-550, 300 hp (224 kW)

[edit] Performance

  • Maximum speed: 253 mph (405 km/h)
  • Range: 2,475 miles (3,960 km)
  • Service ceiling: ft ( m)
  • Rate of climb: 1,600 ft/min (488 m/min)
  • Wing loading: lb/ft² ( kg/m²)
  • Power/mass: hp/lb ( W/kg)

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