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O'Neill Aristocraft II

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Manufacturer
  
O'Niell Aircraft Company

The Aristocraft II was a six-place homebuilt aircraft designed by Terrence O'Neill.

Contents

Design and development

The Aristocraft II was a redesigned aircraft built off the prototype airframe of the WACO Aristocraft. The Franklin-powered Aristocraft pusher was rebuilt using the wings and most of the internal structure of the original. The layout was drastically changed from a twin-tailed, mid-engined, pusher to a conventional tractor arrangement. The intent was to develop a homebuilt aircraft from the design with the flexibility to carry six passengers, or fewer people with extended range. A effort was made to certify the design, under the name Model W Winner but money ran out before completion, with only two orders.

The Aristocraft II was a strut-braced, high-wing, tricycle gear, six-passenger aircraft designed for Franklin or Lycoming 200 hp (149 kW) engines. The fuselage was made of welded steel tubing with aluminum skin. The cowling was split vertically, and could hinge open for maintenance.

Variants

The standard engine was a six-cylinder Lycoming, however plans were drawn for a 245 hp (183 kW) Jacobs L-4MB radial engine installation and also for a Continental R-670 radial installation. This specified that the engine would be mounted closer to the firewall and also incorporated conventional landing gear, a 93 in (236 cm) propeller and the outward appearance of "Mr. Muligan", this evolved into the O'Neill Magnum.

Specifications (Arisocraft II)

Data from Sport Aviation, Air Trails Summer 1971

General characteristics

  • Crew: one
  • Capacity: five passengers
  • Length: 25 ft 10 in (7.87 m)
  • Wingspan: 36 ft 10 in (11.23 m)
  • Height: 8 ft (2.4 m)
  • Wing area: 190 sq ft (18 m2)
  • Airfoil: NACA 4415
  • Empty weight: 1,800 lb (816 kg)
  • Gross weight: 3,300 lb (1,497 kg)
  • Fuel capacity: 76 gal
  • Powerplant: 1 × Lycoming IO-360 four-cylinder, direct-drive, horizontally-opposed, air-cooled, piston aircraft engine, 200 hp (150 kW)
  • Propellers: 2-bladed
  • Maximum speed: 122 kn; 225 km/h (140 mph)
  • Cruise speed: 113 kn; 209 km/h (130 mph)
  • Stall speed: 48 kn; 89 km/h (55 mph)
  • Range: 695 nmi; 1,287 km (800 mi)
  • Service ceiling: 15,000 ft (4,600 m)
  • Rate of climb: 500 ft/min (2.5 m/s)
  • References

    O'Neill Aristocraft II Wikipedia