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, 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

Links:

Send in additions, new information's or corrections you have!

If you have updates, new info, you have found factual error, error in translation, grammar error or only simple typing error. Please let us know! Fill in the form and send it back. Your help is greatly appreciated.

Name:

Email Address:

Comments:

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
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