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Utva 213 Vihor ✕
Manufacturer Ikarbus
Description Utva 213 Vihor was a late 1940s Yugoslavian two-seat advanced trainer.
First Flight 1949-01-01
Entry Into service 1952-01-01
Service End 1961-01-01
Designer Government Factories
Length (m) 11.52
Height (m) 3.58
Cockpit Crew 2
Max Speed (km/h) 362
Min Speed (km/h) 118
Max Ceiling (m) 7000
Armament 2× machine guns; 2× 50 kg (110 lb) or 4× 25 kg (55 lb) bombs
National Origin Yugoslavia
Number Built 196
Powerplant Description 1 × Ranger SVG-770C-1B air-cooled inverted V12 engine, 388 kW (520 hp) each
Primary Users Yugoslav Air Force
Wikipedia Article (URL) en.wikipedia.org/wiki/Utva_213_Vihor
Flat Wing Span (m) 11
Number of Engines 1