Engineering:Alliance A-1 Argo

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A-1 Argo
The sole surviving airworthy A-1 Argo biplane, 1929-built, at the Golden Wings Air Museum at Anoka near Minneapolis, Minnesota.
General information
Typeprivate owner biplane
National originUnited States
ManufacturerAlliance Aircraft Corporation
Number built20
History
First flight1929

The Alliance A-1 Argo was an American-built two-seat biplane of the late 1920s.

Development

The Alliance Aircraft Corporation of Alliance, Ohio, was formed in 1928 by a reorganization of the Hess Aircraft Co. The firm designed the A-1 Argo as a sturdy two-seat open-cockpit biplane for operation by private pilot owners. The Warrior seven-cylinder engine was designed and produced in the same factory at Alliance.[1]

Operational history

Because of the difficult economic climate then existing, only 20 A-1 Argos were completed. Alliance Aircraft then went into bankruptcy in 1930, being reformed briefly as the Warrior Aeronautical Corporation before that organization also foundered later the same year.[1]

Several Argo biplanes continued in operation by private owners until curtailment of civil flying in the USA in 1941. Two aircraft survived in mid-2009 of which, NC2M (N2M) was rebuilt to airworthy condition by Greg Herrick's Golden Wings Air Museum.

The Ohio History Connection displays a static A-1 Argo on the plaza level of the Ohio History Center. This particular aircraft was constructed in August 1929.[2]


Specifications

Data from Manufacturer's Specifications on American Commercial Airplanes as compiled by Aviation[3]

General characteristics

  • Crew: 1
  • Capacity: 1 passenger
  • Length: 20 ft 2 in (6.15 m)
  • Wingspan: 28 ft 8 in (8.74 m)
  • Height: 8 ft 0 in (2.44 m)
  • Wing area: 203 sq ft (18.9 m2)
  • Empty weight: 1,077 lb (489 kg)
  • Gross weight: 1,615 lb (733 kg)
  • Fuel capacity: 35 US gal (29 imp gal; 130 L)
  • Powerplant: 1 × Hess Warrior seven-cylinder radial[4] , 115 hp (86 kW)

Performance

  • Maximum speed: 125 mph (201 km/h, 109 kn)
  • Cruise speed: 100 mph (164 km/h, 87 kn)
  • Stall speed: 40 mph (71 km/h, 35 kn) (landing speed)
  • Range: 425 mi (684 km, 369 nmi)
  • Service ceiling: 16,000 ft (4,900 m)
  • Rate of climb: 1,050 ft/min (5.3 m/s)

See also

References

Notes
Bibliography