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Historical Ryan STA

From Wikipedia, the free encyclopedia
American light aircraft

Ryan STA
The prototype Historical Ryan STA on display
General information
TypeHomebuilt aircraft
National originUnited States
ManufacturerHistorical Aircraft Corporation
StatusProduction completed
Number builtOne
History
Introduction date1997
Developed fromRyan STA

TheHistorical Ryan STA was an Americanhomebuilt aircraft that was designed and produced by theHistorical Aircraft Corporation ofNucla, Colorado. The aircraft was an 85% scale replica of the originalRyan STA and when it was available was supplied as a kit for amateur construction.[1]

Design and development

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The aircraft featured awire-braced andstrut-bracedlow-wing, two seats in separatetandem open cockpits with windshields, fixedconventional landing gear and a single engine intractor configuration.[1]

The aircraftfuselage was made from welded steel tubing, while the wings had woodenspars andribs covered indopedaircraft fabric. Several prefabricated components were supplied as part of the kit, including the fuselage frame,landing gear, engine mount and tail assembly. The manufacturer rated the STA kit as suitable for beginners and estimated the construction time from the supplied kit as 1500 hours. The kit could be completed to represent an STA, a militaryPT-16 or aPT-20.[1]

The aircraft's 26.00 ft (7.9 m) span wing had an area of 112.6 sq ft (10.46 m2). The cockpit width was 22 in (56 cm) and the standard engine used was the 100 hp (75 kW)CAM 100 powerplant. It had a typical empty weight of 725 lb (329 kg) and a gross weight of 1,275 lb (578 kg), giving a useful load of 500 lb (230 kg). With full fuel of 23 U.S. gallons (87 L; 19 imp gal) the payload for pilot, passenger and baggage was 362 lb (164 kg).[1]

Operational history

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In January 2014 no examples remainedregistered in the United States with theFederal Aviation Administration. Although one aircraft had been registered in 1997, it was listed as destroyed and deregistered in 2002. It is likely that no examples exist today.[2]

Specifications (STA)

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Data from AeroCrafter[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 20.10 ft (6.13 m)
  • Wingspan: 26.00 ft (7.92 m)
  • Wing area: 112.6 sq ft (10.46 m2)
  • Empty weight: 725 lb (329 kg)
  • Gross weight: 1,275 lb (578 kg)
  • Fuel capacity: 23 U.S. gallons (87 L; 19 imp gal)
  • Powerplant: 1 ×CAM 100 four cylinderfour strokeaircraft engine, 100 hp (75 kW)
  • Propellers: 2-bladed fixed pitch wooden

Performance

  • Maximum speed: 125 mph (201 km/h, 109 kn)
  • Cruise speed: 110 mph (180 km/h, 96 kn)
  • Stall speed: 53 mph (85 km/h, 46 kn)
  • Range: 490 mi (790 km, 430 nmi)
  • Service ceiling: 16,300 ft (5,000 m)
  • Rate of climb: 930 ft/min (4.7 m/s)
  • Wing loading: 11.3 lb/sq ft (55 kg/m2)

References

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  1. ^abcdePurdy, Don:AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 178. BAI Communications, 15 July 1998.ISBN 0-9636409-4-1
  2. ^Federal Aviation Administration (January 2, 2014)."Make / Model Inquiry Results". RetrievedJanuary 2, 2014.
Homebuilt aircraft
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