The Utva C-3 Trojka (Trey) was a light aircraft built in Yugoslavia shortly after World War II as a result of a government competition to develop a new, domestically built aircraft with which to equip the country's flying clubs. The winning design was submitted by and and the prototype was built by Ikarus as the Ikarus 251. Series production took place at Utva as the C-3. It was a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage. The pilot and instructor sat side by side under an expansive canopy. The type remained in production until the mid-1950s with later examples powered by the more powerful Walter Mikron 4.
Attributes | Values |
---|---|
rdf:type | |
rdfs:label |
|
rdfs:comment |
|
foaf:depiction | |
dcterms:subject | |
Wikipage page ID |
|
Wikipage revision ID |
|
Link from a Wikipage to another Wikipage |
|
sameAs | |
similar aircraft |
|
span ft |
|
span in |
|
span m |
|
wing area sqft |
|
wing area sqm |
|
dbp:wikiPageUsesTemplate | |
thumbnail | |
dbp:primeUnits%3F_ |
|
first flight |
|
national origin |
|
crew |
|
height ft |
|
height in |
|
length ft |
|
manufacturer | |
type |
|
has abstract |
|
ceiling ft |
|
ceiling m |
|
empty weight kg |
|
empty weight lb |
|
eng1 hp |
|
eng1 kw |
|
eng1 name |
|
eng1 number |
|
gross weight kg |
|
gross weight lb |
|
height m |
|
length in |
|
length m |
|
max speed kmh |
|