avia.wikisort.org - Aeroplane
The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding by Aircraft Designs Inc.[1][2][3]
| Stallion | |
|---|---|
 | |
| Role | Light utility aircraft |
| National origin | United States of America |
| Manufacturer | Aircraft Designs Inc |
| Designer | Martin Hollmann |
| First flight | July 1994 |
| Number built | 7 (2007) |
Design and development
The Stallion is a single-engined high-winged monoplane, with wings based on those of the Lancair ES and a retractable tricycle landing gear from the Lancair IV. It has a steel-tube fuselage center section, with the remainder of the airframe of composite construction, and is designed to be powered by engines of 230–350 hp (172–261 kW). The recommended engine is the 300 hp (224 kW) Continental IO-550, but engines as powerful as the 750 hp (559 kW) Walter M601 have been used.[1][3][4] It is available in two versions, the four seat ADI Stallion and the six-seat Super Stallion.[3][5]
Operational history
Seven examples had been completed and flown by December 2007.[2]
Specifications (ADI Super Stallion – 350 hp engine)
Data from Jane's All The World's Aircraft 2003–2004.[4]
General characteristics
- Crew: one pilot
- Capacity: 5 passengers
- Length: 25 ft 0 in (7.62 m)
- Wingspan: 35 ft 0 in (10.67 m)
- Height: 9 ft 6 in (2.90 m)
- Wing area: 140.1 sq ft (13.00 m2)
- Aspect ratio: 8.8:1
- Empty weight: 2,200 lb (998 kg)
- Max takeoff weight: 3,800 lb (1,784 kg)
- Powerplant: 1 × Continental TSIO-550-B air-cooled turbocharged flat-six engine, 350 hp (224 kW)
Performance
- Maximum speed: 306 mph (493 km/h, 266 kn)
- Cruise speed: 295 mph (474 km/h, 256 kn)
- Stall speed: 71 mph (115 km/h, 62 kn)
- Range: 2,700 mi (4,345 km, 2,346 nmi)
- Service ceiling: 32,000 ft (9,750 m)
- Rate of climb: 2,600 ft/min (13.2 m/s)
See also
Related development
References
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 91. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- Downey, Julia: 2008 Kit Aircraft Directory, Kitplanes, Volume 24, Number 12, December 2007, page 38. Primedia Publications. ISSN 0891-1851
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015–16, page 94. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Jackson 2003, pp. 499–500.
- Taylor 1999, p. 560.
- Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.
- Taylor, Michael. Brassey's World Aircraft & Systems Directory 1999/2000. London: Brasseys, 1999. ISBN 1-85753-245-7.
На других языках
- [en] ADI Stallion
[fr] ADI Stallion
L'ADI Stallion est un quadriplace utilitaire dont le prototype [N408S] a effectué son premier vol en 1994. C'est un monoplan à aile haute cantilever et train tricycle escamotable de construction composite. Cet appareil peut transporter jusqu’à 6 personnes, à condition de supprimer le coffre à bagages à l’arrière de la cabine et devient Super Stallion avec un moteur Continental TSIO-550-E. Le Stallion est commercialisé en kit par Aircraft Designs Inc et plusieurs exemplaires étaient en construction aux États-Unis et en Nouvelle-Zélande début 2001. Aucun n’avait encore obtenu de certification en janvier 2007.Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
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