{{Short description|US civil utility aircraft}} {{Infobox aircraft |name =Stallion |image=File:2004 Hollmann Super Stallion.jpg |caption= |alt= |type= Light utility aircraft |national_origin=United States of America |manufacturer=Aircraft Designs Inc |designer=Martin Hollmann |first_flight =July 1994 |number_built = 7 (2007) }} 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.<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011–12'', page 91. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref><ref name="KitplanesDec2007">Downey, Julia: ''2008 Kit Aircraft Directory'', Kitplanes, Volume 24, Number 12, December 2007, page 38. Primedia Publications. ISSN 0891-1851</ref><ref name="WDLA15">Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015–16'', page 94. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}</ref>
==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 {{convert|300|hp|kW|0|abbr=on}} Continental IO-550, but engines as powerful as the {{convert|750|hp|kW|0|abbr=on}} Walter M601 have been used.<ref name="WDLA11"/><ref name="WDLA15"/><ref name="JAWA p499-0">Jackson 2003, pp. 499–500.</ref> It is available in two versions, the four seat ADI Stallion and the six-seat Super Stallion.<ref name="WDLA15"/><ref name="Brasseys99 p560">Taylor 1999, p. 560.</ref>
==Operational history== Seven examples had been completed and flown by December 2007.<ref name="KitplanesDec2007"/>
==Specifications (ADI Super Stallion – 350 hp engine)== {{Aircraft specs |prime units?=imp |ref=''Jane's All The World's Aircraft 2003–2004.''<ref name="JAWA p499-0"/> |crew= one pilot |capacity=5 passengers |length ft= 25 |length in= 0 |length m= 7.62 |span ft= 35 |span in= 0 |span m= 10.67 |height ft= 9 |height in= 6 |height m= 2.90 |wing area sqft= 140.1 |wing area sqm= 13.00 |aspect ratio=8.8:1 |empty weight lb= 2200 |empty weight kg= 998 |max takeoff weight lb=3800 |max takeoff weight kg= 1784 |eng1 name= Continental TSIO-550-B |eng1 type=air-cooled turbocharged flat-six engine |eng1 number=1 |eng1 hp= 350 |eng1 kw= 224 |max speed mph= 306 |max speed kts=266 |max speed kmh=493 |cruise speed mph= 295 |cruise speed kts=256 |cruise speed kmh=474 |stall speed mph= 71 |stall speed kts= 62 |stall speed kmh= 115 |range miles=2700 |range nmi=2346 |range km=4345 |ceiling ft= 32000 |ceiling m= 9750 |climb rate ftmin= 2600 |climb rate ms= 13.2 |avionics= }}
==See also== {{Aircontent |related=*Lancair IV |similar aircraft= |lists= |see also= }}
==References== {{Reflist}}
* 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}}. {{ADI aircraft}}
{{DEFAULTSORT:Adi Stallion}} Category:Single-engined tractor aircraft Category:High-wing aircraft Category:Homebuilt aircraft Category:1990s United States civil utility aircraft Stallion Category:Aircraft with retractable tricycle landing gear