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.
Specifications (ADI Stallion)
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)
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)
Related content
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