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词条 Aeroprakt A-28 Victor
释义

  1. Design and development

  2. Operational history

  3. Specifications (A-28 Victor)

  4. References

  5. External links

name=Aeroprakt A-28 Victor image=File:Aeroprakt A28 Victor 01.JPG caption=

}}{{Infobox Aircraft Type

 type=Light aircraft national origin=Ukraine manufacturer=Aeroprakt designer= first flight= introduced= retired= status=In production (2011) primary user= more users= produced= number built=at least three program cost= unit cost= developed from= variants with their own articles=
}}

The Aeroprakt A-28 Victor is a Ukrainian light aircraft, designed and produced by Aeroprakt of Kiev. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

Design and development

The design goals for the A-28 included twin engines for safety over hazardous terrain, a payload of {{convert|300|kg|lb|abbr=on}} with four seats, 10 hours endurance, as well as good short and rough field capabilities. The resulting design features a cantilever low-wing, a four-seat enclosed cabin accessed through a hinged windshield, a T-tail, fixed conventional landing gear and twin engines in tractor configuration.[1]

The aircraft has mixed construction, with the forward fuselage made from fibreglass and the tail cone of aluminum sheet. The wings and tail are all-aluminum, while the control surfaces are aluminum frames covered in doped aircraft fabric. Its {{convert|12|m|ft|1|abbr=on}} span wing employs a TsAGI P-IIIA-15 airfoil, has an area of {{convert|13.4|m2|sqft|abbr=on}} and mounts flaps. The standard engines fitted are two {{convert|80|hp|kW|0|abbr=on}} Rotax 912 or two {{convert|100|hp|kW|0|abbr=on}} Rotax 912S powerplants. The conventional landing gear fits wheel pants and features a steerable tailwheel.[1][2]

The A-28 has an empty weight of {{convert|530|kg|lb|abbr=on}} and a gross weight of {{convert|1100|kg|lb|abbr=on}}, giving a useful load of {{convert|570|kg|lb|abbr=on}}.[1]

Operational history

One example was registered in 2001 in the United States with the Federal Aviation Administration in the amateur-built category, but on 18 October 2004 it was deregistered and exported to Ukraine.[3][4]

Specifications (A-28 Victor)

{{Aircraft specs
|ref=Bayerl[1]
|prime units?=met


|genhide=
|crew=one
|capacity=three passengers
|length m=
|length ft=
|length in=
|length note=
|span m=12
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=13.4
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=TsAGI P-IIIA-15
|empty weight kg=530
|empty weight lb=
|empty weight note=
|gross weight kg=1100
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|180|l}}
|more general=


|eng1 number=2
|eng1 name=Rotax 912
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=60
|eng1 hp=
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=300
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=250
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=90
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=5
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=82.1
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 154. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 18 December 2012|last = Lednicer |first = David |authorlink = |year = 2010}}
3. ^{{cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=A-28+VICTOR&PageNo=1|title = Make / Model Inquiry Results|accessdate = 18 December 2012|last = Federal Aviation Administration|date = 18 December 2012}}
4. ^{{cite web|url = http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=61450|title = Registration Inquiry Results - N61450|accessdate = 18 December 2012|last = Federal Aviation Administration|date = 18 December 2012}}

External links

  • {{Official website|http://aeroprakt.kiev.ua/airplanes/about/id/10}} (in Ukrainian)
  • Official photo gallery (in Ukrainian)
{{Commons category|Aeroprakt A-28}}{{Aeroprakt aircraft}}

5 : Twin-engined tractor aircraft|Aeroprakt aircraft|Low-wing aircraft|Ukrainian civil aircraft 2000–2009|T-tail aircraft
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