- Development
- Specifications
- See also
- References Notes Bibliography
| name=C-1 Cadet | image=AeroncaC-2CF-AOR.jpg | caption=An Aeronca C-2 which was similar to the C-1 Cadet }}{{Infobox Aircraft Type | type=Single-seat light sport aircraft | national origin=United States | manufacturer=Aeronca | designer= | first flight=1931 | introduced= | retired= | status= | primary user= | number built=3 | developed from= | variants with their own articles=
}} |
The Aeronca C-1 Cadet was a high performance version of the Aeronca C-2 developed by Aeronca and first flown in 1931. DevelopmentThe C-1 was a wire-braced high-wing monoplane with a fixed tail skid landing gear and powered by a {{convert|36|hp|kW|0|abbr=on}} Aeronca E-113 flat-twin piston engine. Specifications{{Aircraft specs
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|crew=1
|capacity=
|length m=
|length ft=
|length in=
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|span m=
|span ft=29
|span in=0
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|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=115
|wing area note=
|empty weight kg=
|empty weight lb=426
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=700
|max takeoff weight note=
|more general=
|eng1 number=1
|eng1 name=Aeronca E-113
|eng1 type=flat-twin piston
|eng1 kw=
|eng1 hp=36
|power original=
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|max speed kmh=
|max speed mph=95
|max speed kts=
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|cruise speed kmh=
|cruise speed mph=80
|cruise speed kts=
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|never exceed speed kmh=
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|range km=
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|range note=
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|ceiling m=
|ceiling ft=12500
|ceiling note=
|climb rate ms=
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|climb rate note=
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See also{{aircontent
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}}ReferencesNotes
}}Bibliography{{refbegin}}- {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}}{{Aeronca}} 5 : United States civil utility aircraft 1930–1939|Aeronca aircraft|High-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1931 |