Falconar AMF-S14

__NOTOC__ Infobox Aircraft
name=AMF-S14 Maranda


caption=
type=Utility aircraft
manufacturer=Homebuilt
designer=Chris Falconar
first flight=avyear|1961
introduced=
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variants with their own articles=The Falconar AMF-S14 Maranda is a two-seat light aircraft first flown in Canada in 1961 and marketed for homebuilding. Based on the Adam RA-14 Loisirs, it is a conventional high-wing strut-braced monoplane with fixed, tailwheel undercarriage. The pilot and single passenger sit side-by-side in a fully enclosed cabin.

pecifications (typical Super Maranda)

aerospecs
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crew=One pilot
capacity=1 passenger
length m=6.70
length ft=22
length in=0
span m=9.67
span ft=31
span in=9
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wing area sqm=14.7
wing area sqft=158
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aspect ratio=
empty weight kg=500
empty weight lb=1,100
gross weight kg=840
gross weight lb=1,850
lift kg=
lift lb=

eng1 number=1
eng1 type=Lycoming O-320 four-cylinder horizontally-opposed air-cooled piston engine
eng1 kw= 112
eng1 hp= 150
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max speed kmh=
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max speed mach=
cruise speed kmh= 193
cruise speed mph= 120
range km=770
range miles=480
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References

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* [http://www.falconaravia.com/ Plan vendor's website]