The UTVA-60 is a Yugoslavian light aircraft of the 1960s. First flying in 1959, it was built by UTVA for both the Yugoslavian armed forces and for civilian use.
| Attributes | Values |
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| rdf:type | |
| rdfs:label |
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| rdfs:comment |
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| sameAs | |
| empty weight kg |
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| dcterms:subject | |
| dbkwik:military/pr...iPageUsesTemplate |
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| prop blade number |
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| airfoil |
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| range km |
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| ceiling ft |
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| climb rate ftmin |
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| stall speed kmh |
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| max takeoff weight lb |
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| never exceed speed kmh |
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| eng1 type |
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| length in |
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| Introduced |
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| Type |
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| max speed note |
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| eng1 kW |
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| wing area sqft |
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| height m |
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| Height in |
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| span m |
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| climb rate ms |
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| wing loading kg/m |
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| wing loading lb/sqft |
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| Manufacturer | |
| max speed kmh |
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| empty weight lb |
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| Capacity |
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| ceiling m |
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| cruise speed kmh |
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| length m |
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| National Origin |
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| aspect ratio |
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| length ft |
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| Height ft |
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| First Flight |
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| span ft |
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| max takeoff weight kg |
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| span in |
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| wing area sqm |
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| prime units? |
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| variants with their own articles | |
| prop name |
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| Crew |
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| eng1 name |
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| eng1 hp |
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| ref |
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| eng1 number |
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| abstract |
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