About: Legrand-Simon LS.60     Goto   Sponge   NotDistinct   Permalink

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The Legrand-Simon LS.60 is a single-engine, high-wing monoplane seating two side-by-side. It was built in France in the early 1960s in response to a government competition for a club trainer. It won the competition but nevertheless failed to go into production; only the prototype, which still flies, was completed.

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  • Legrand-Simon LS.60 (en)
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  • The Legrand-Simon LS.60 is a single-engine, high-wing monoplane seating two side-by-side. It was built in France in the early 1960s in response to a government competition for a club trainer. It won the competition but nevertheless failed to go into production; only the prototype, which still flies, was completed. (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/Legrand_Simon_LS60_F-BJSA_GUY_16.06.63_edited-2.jpg
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  • https://web.archive.org/web/20121009053731/http:/www.ae.illinois.edu/m-selig/ads/afplots/naca23012.gif
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span m
wing area sqm
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  • met (en)
first flight
national origin
capacity
designer
  • Paul Legrand and Michel Simon (en)
ref
  • Jane's All the World's Aircraft 1962-63 (en)
type
  • Two seat light aircraft (en)
has abstract
  • The Legrand-Simon LS.60 is a single-engine, high-wing monoplane seating two side-by-side. It was built in France in the early 1960s in response to a government competition for a club trainer. It won the competition but nevertheless failed to go into production; only the prototype, which still flies, was completed. (en)
airfoil
aspect ratio
ceiling m
ceiling note
  • service (en)
climb rate ms
climb rate note
  • at sea level (en)
cruise speed kmh
cruise speed note
developed from
  • LS.50 Dauphine (en)
empty weight kg
eng1 hp
eng1 name
  • Continental C90-14F (en)
eng1 number
eng1 type
  • Air cooled flat four (en)
length m
max speed kmh
max speed note
  • at sea level (en)
max takeoff weight kg
more performance
number built
prop blade number
prop name
  • Ratier, pitch ground adjustable (en)
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