Prijem
UTVA-75
Role: Primary/basic flying training with limited armament training and counter-insurgency capabilities
First flown: May 1976
Manufacture: UTVA - SOUR Metalne Industrije, ro Fabrika Aviona, Pančevo
UTVA - SOUR Metal Industry, Aircraft Factory, Pancevo
Used by: Yugoslavia/Serbia UTVA-75 V-53 130 1980-curr
Croatia
Technical data
UTVA-75A21 UTVA-75A41
Wing span: 9.73 meters (31 ft 11 in)
Length: 7.11 meters (23 ft 4in)
Height: 3.149 meters (10 ft 4 in)
Wing area: 14.63 sq meters (157.48 sq ft)
Crew: Pupil and Pilot side by side
Take-off weight: 960 kg 1163 kg (2,564 lb)
Empty weight: 685 kg 700 kg (1,544 lb)
Weapon load: 200 kg (441 lb)
Internal fuel load: 103 kg (150 litre; 227 lb)
External fuel load: up to 153 kg (337 lb) in two 100 litre (26.4 US Gal or 22 Imp gal) drop tanks
Maximum speed: 215 km/h (133 mph or 116 kt) at meters ( ft) 210 km/h (130 mph or 113 kt)
Cruising speed: 185 km/h (115 mph or 100 kt) at meters ( ft) 180 km/h (112 mph or 97 kt)
Economical speed: 165 km/h (102 mph or 89 kt) 160 km/h (99 mph or 86 kt)
Minimal speed: 82 km/h
Maximum range: 800 km (497 miles or 432 nm)
Ferry range 2,000 km (1,242 miles or 1,079 nm) with drop tanks
Ceiling: 4,000 meters (13,125 ft)
Rate of climb: 270 meters (886 ft) per minute at sea level
4.6 m/s 264 meters (866 ft) per minute at sea level
G limit: -3 to +6
Radar: None
Targeting: optical sight
Engines: One Textron Lycoming I0-360-B1F flat-four piston engine rated at 180 hp (134 kW)
Weapons
Disposable
two hard points - all under the wings
100 kg 100 kg
(220 lb) (220 lb)
machine-gun pod machine-gun pod
Rocket pod with 2 unguided rockets Rocket pod with 2 unguided rockets
Variants
UTVA-75A21 two-seater with dual controls and provisions for blind instrument flying
UTVA-75A41 advanced avionics, first flown in 1986, in production 1987
Role: Primary/basic flying training with limited armament training and counter-insurgency capabilities
First flown: May 1976
Manufacture: UTVA - SOUR Metalne Industrije, ro Fabrika Aviona, Pančevo
UTVA - SOUR Metal Industry, Aircraft Factory, Pancevo
Used by: Yugoslavia/Serbia UTVA-75 V-53 130 1980-curr
Croatia
Technical data
UTVA-75A21 UTVA-75A41
Wing span: 9.73 meters (31 ft 11 in)
Length: 7.11 meters (23 ft 4in)
Height: 3.149 meters (10 ft 4 in)
Wing area: 14.63 sq meters (157.48 sq ft)
Crew: Pupil and Pilot side by side
Take-off weight: 960 kg 1163 kg (2,564 lb)
Empty weight: 685 kg 700 kg (1,544 lb)
Weapon load: 200 kg (441 lb)
Internal fuel load: 103 kg (150 litre; 227 lb)
External fuel load: up to 153 kg (337 lb) in two 100 litre (26.4 US Gal or 22 Imp gal) drop tanks
Maximum speed: 215 km/h (133 mph or 116 kt) at meters ( ft) 210 km/h (130 mph or 113 kt)
Cruising speed: 185 km/h (115 mph or 100 kt) at meters ( ft) 180 km/h (112 mph or 97 kt)
Economical speed: 165 km/h (102 mph or 89 kt) 160 km/h (99 mph or 86 kt)
Minimal speed: 82 km/h
Maximum range: 800 km (497 miles or 432 nm)
Ferry range 2,000 km (1,242 miles or 1,079 nm) with drop tanks
Ceiling: 4,000 meters (13,125 ft)
Rate of climb: 270 meters (886 ft) per minute at sea level
4.6 m/s 264 meters (866 ft) per minute at sea level
G limit: -3 to +6
Radar: None
Targeting: optical sight
Engines: One Textron Lycoming I0-360-B1F flat-four piston engine rated at 180 hp (134 kW)
Weapons
Disposable
two hard points - all under the wings
100 kg 100 kg
(220 lb) (220 lb)
machine-gun pod machine-gun pod
Rocket pod with 2 unguided rockets Rocket pod with 2 unguided rockets
Variants
UTVA-75A21 two-seater with dual controls and provisions for blind instrument flying
UTVA-75A41 advanced avionics, first flown in 1986, in production 1987
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