UTVA-75

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, PanÄevo
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

Links:

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, PanÄevo UTVA - SOUR Metal Industry, Aircraft Factory, Pancevo
Used by:	Yugoslavia/Serbia	UTVA-75 V-53	130	1980-curr
Used by:	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