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About: dbkwik:resource/Gg-yA59MsnqWTTmY5iDQuA==

PropertyValue
rdf:type
rdfs:label
  • UTVA-60
rdfs:comment
  • 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.
owl:sameAs
empty weight kg
  • 952
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
prop blade number
  • 2
airfoil
  • NACA 4412
range km
  • 780
ceiling ft
  • 17060
climb rate ftmin
  • 1260
stall speed kmh
  • 73
max takeoff weight lb
  • 3571
never exceed speed kmh
  • 300
eng1 type
  • air-cooled flat-six
length in
  • 11
Introduced
  • 1960
Type
  • Light utility/training aircraft
max speed note
  • at sea level
eng1 kW
  • 201
wing area sqft
  • 194.620000
height m
  • 2.720000
Height in
  • 11
span m
  • 11.400000
climb rate ms
  • 6.400000
wing loading kg/m
  • 89.600000
wing loading lb/sqft
  • 18.350000
Manufacturer
max speed kmh
  • 252
empty weight lb
  • 2099
Capacity
  • 3
ceiling m
  • 5200
cruise speed kmh
  • 230
length m
  • 8.220000
National Origin
  • Yugoslavia
aspect ratio
  • 7.190000
length ft
  • 26
Height ft
  • 8
First Flight
  • 1959-04-22
span ft
  • 37
max takeoff weight kg
  • 1620
span in
  • 4
wing area sqm
  • 18.080000
prime units?
  • met
variants with their own articles
prop name
  • Hartzell HC-A2X20-1B/10133-3 constant speed metal propeller
Crew
  • 1
eng1 name
  • Lycoming O-480-G1H6
eng1 hp
  • 270
ref
  • Jane's All The World's Aircraft 1965-66; Mondey
eng1 number
  • 1
abstract
  • 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.