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The Renard R.30 was a prototype trimotor airliner built in Belgium in 1931. It was a strut-braced high-wing monoplane of conventional design with a fully enclosed flight deck and separate passenger compartment. One engine was mounted on the nose, while the other two were mounted on the leading edges of the wings. Construction was metal throughout, skinned in plywood and fabric.

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  • Renard R-30 (fr)
  • Renard R.30 (en)
rdfs:comment
  • Le Renard R-30 est un avion léger trimoteur resté à l'état de prototype construit par l'avionneur belge Renard Constructions Aéronautiques. (fr)
  • The Renard R.30 was a prototype trimotor airliner built in Belgium in 1931. It was a strut-braced high-wing monoplane of conventional design with a fully enclosed flight deck and separate passenger compartment. One engine was mounted on the nose, while the other two were mounted on the leading edges of the wings. Construction was metal throughout, skinned in plywood and fabric. (en)
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span m
stall speed kmh
time to altitude
wing area sqm
wing loading kg/m
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  • met (en)
first flight
national origin
  • Belgium (en)
capacity
crew
manufacturer
ref
  • Jane's all the World's Aircraft 1931 (en)
type
  • Airliner (en)
has abstract
  • Le Renard R-30 est un avion léger trimoteur resté à l'état de prototype construit par l'avionneur belge Renard Constructions Aéronautiques. (fr)
  • The Renard R.30 was a prototype trimotor airliner built in Belgium in 1931. It was a strut-braced high-wing monoplane of conventional design with a fully enclosed flight deck and separate passenger compartment. One engine was mounted on the nose, while the other two were mounted on the leading edges of the wings. Construction was metal throughout, skinned in plywood and fabric. The R.30 was designed in response to a Belgian government requirement of 1929 for a long-range passenger transport aircraft to service Belgian Congo. The design met the specifications laid down, but by the time it flew in 1931, it was judged already obsolete. The single prototype, registered OO-AMK, was the only example built. (en)
ceiling m
climb rate ms
empty weight kg
eng1 hp
eng1 name
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  • at 1,750 rpm; at 1900 rpm for take-off (en)
eng1 number
eng1 type
gross weight kg
height m
length m
max speed kmh
number built
prop blade number
prop dia m
prop name
  • wooden fixed-pitch propellers (en)
range km
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page length (characters) of wiki page
number built
manufacturer
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is Link from a Wikipage to another Wikipage of
is foaf:primaryTopic of
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