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词条 Criquet Storch
释义

  1. Design and development

  2. Specifications (version)

  3. See also

  4. References

name=Storch image= caption=

}}{{Infobox Aircraft Type

 type=Light-sport aircraft national origin=Colombia manufacturer=Criquet Aviation designer= first flight= introduced= retired= status=Production completed primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Criquet Storch ({{lang-en|Stork}}) is a Colombian light-sport aircraft that was designed and produced by Criquet Aviation of Guaymaral Airport, Bogotá. The aircraft is a 75% scale replica of the German Second World War STOL liaison aircraft, the Fieseler Fi 156 Storch, with the company named for the French post-war production model of the same aircraft, the Morane-Saulnier MS.505 Criquet.[1][2]

Design and development

The aircraft was adapted from the original German plans to comply with the US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-tandem enclosed cockpit, fixed conventional landing gear and a single engine in tractor configuration.[1][2]

The aircraft's {{convert|10.5|m|ft|1|abbr=on}} span wing has an area of {{convert|16|m2|sqft|abbr=on}} and is equipped with flaps and leading edge slots. Standard engines that were available include the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS, {{convert|115|hp|kW|0|abbr=on}} turbocharged Rotax 914, {{convert|110|hp|kW|0|abbr=on}} Rotec R2800, {{convert|150|hp|kW|0|abbr=on}} Rotec R3600 radial engine and the {{convert|108|hp|kW|0|abbr=on}} Lycoming O-235 four-stroke powerplants.[1][2]

The design is an accepted Federal Aviation Administration Special Light-sport Aircraft.[3]

Specifications (version)

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


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=10.5
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=16
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=385
|empty weight lb=
|empty weight note=
|gross weight kg=625
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|110|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 912ULS
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=75
|eng1 hp=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=130
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=40
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=190
|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=
|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=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

See also

  • Carlson Criquet
  • Pazmany PL-9 Stork
  • RagWing RW19 Stork

References

1. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 38. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^1 2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 41. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
3. ^{{cite web|url = https://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xlsx|title = SLSA Make/Model Directory|accessdate = 5 February 2017|last = Federal Aviation Administration|date = 26 September 2016}}

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