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The SFCA Maillet 20 was a French three seat tourer built in 1935. The Armée de l'Air ordered 30 for training and liaison and several were raced. The aircraft was developed through 1935 via cockpit layout and canopy changes to the provision of retracting landing gear.

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rdf:type
rdfs:label
  • SFCA Maillet 20 (en)
rdfs:comment
  • The SFCA Maillet 20 was a French three seat tourer built in 1935. The Armée de l'Air ordered 30 for training and liaison and several were raced. The aircraft was developed through 1935 via cockpit layout and canopy changes to the provision of retracting landing gear. (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/SFCA_Maillet_20_photo_L'Aerophile_April_1935.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/SFCA_Maillet-21-Spanish_Republican_AF.jpg
dct:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
sameAs
span m
wing area sqm
dbp:wikiPageUsesTemplate
thumbnail
dbp:primeUnits%3F_
  • met (en)
first flight
national origin
capacity
  • Two passengers (en)
crew
  • One (en)
designer
  • Jean Lignel (en)
fuel capacity
  • fuel plus oil (en)
manufacturer
ref
  • L'Année Aéronautique 1934–1935, p.22 (en)
type
  • Three seat tourer (en)
has abstract
  • The SFCA Maillet 20 was a French three seat tourer built in 1935. The Armée de l'Air ordered 30 for training and liaison and several were raced. The aircraft was developed through 1935 via cockpit layout and canopy changes to the provision of retracting landing gear. (en)
ceiling m
climb rate ms
climb rate note
  • initial (en)
cruise speed kmh
cruise speed note
  • at 80% power (en)
empty weight kg
eng1 hp
eng1 name
eng1 number
eng1 type
  • air cooled, inverted six-cylinder inline (en)
gross weight kg
height m
length m
max speed kmh
max speed note
  • at ground level (en)
more performance
  • * Landing speed: (en)
number built
  • c.37 (en)
prop blade number
prop dia m
prop name
range km
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