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UTVA-66 Short takeoff and landing aircraft

UTVA-66 Short takeoff  and landing aircraft. First flight: 1968 © Konstantinos Panitsidis
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Manufacturer: UTVA
Country: Yugoslavia
First flight: 1968
Type: Short takeoff  and landing aircraft (STOL)

Abbreviation FYROM - the Former Yugoslav Republic of Makedonia


 The only UTVA-66 of the Air Force FYROM, at the static exhibition Air Show Bitola 2011, the plane is probably out of order. A light multipurpose three-seater aircraft with piston engine, Lycoming GSO-480-B1A6 (J6) takeoff power 340 h.p., developed on the basis of the UTVA-60 at the end of the 60s by the Yugoslav company UTVA (Fabrica Aviona Utva). The first flight took place in 1968. A total of 130 units were produced and has been exported to countries such as to France, Ireland, Canada, the USA and the countries of the former Yugoslavia.

Aircraft modifications: UTVA-66-AM ambulance, UTVA-66H float seaplane and UTVA-66 (V-52) military modification based on UTVA-66A. 

 

The aircraft with registration number Z3-DCB, sn 51101, took part in the hostilities of the Albanian uprising in Tetov in 2001, static exhibition, Monastery airfield 2011 © Konstantinos Panitsidis
The aircraft with registration number Z3-DCB, sn 51101, took part in the hostilities of the Albanian uprising in Tetov in 2001, static exhibition, Monastery airfield 2011. 

 

UTVA-66 - ένα μέρος του οριζοντίου πτερώματος με πλήγμα από ελαφρά πυρά κατά τις πολεμικές επιχειρήσεις του 2001. Στατική έκθεση, Αεροδρόμιο του Μοναστηρίου 2011 © Konstantinos Panitsidis

UTVA-66 Tail unit, horizontal stabilizer, clearly visible the holes received during the 2001 hostilities, static exhibition, Monastery airfield 2011. 

 

Κοντινή λήψη του εμπρόσθιου τμήματος του προωθητικού συστήματος το οποίο κινεί μια τρίφυλλη έλικα της Hartzell. Στατική έκθεση, αεροδρόμιο του Μοναστηρίου 2011 © Konstantinos Panitsidis

Powerplant Lycoming GSO-480-B1A6 (J6) takeoff power 340 hp. with three-blade propeller Hartzell HC-B3Z20-1 / 10151C-5, static exhibition, Monastery airfield 2011. 




Three-view drawing

UTVA-66 © Konstantinos Panitsidis





Technical specifications

DESIGNER UTVA
COUNTRY Yugoslavia
TYPE
Short takeoff  and landing aircraft
CREW 1
POWER-PLANT One piston engine Textron Lycoming GSO-480-B1A6 (J6)
Power, h.p. 1x340
DIMENSIONS
 
Length, m
8,38
Height, m
3,20
Wing span, m
11,40
Wing area, m2
18,08
WEIGHT  
Maximum take-off, kg 1.748
Normal take-off, kg -
Empty aircraft, kg 1.207
Internal fuel, l -
Payload, kg Transfer 3 passengers
Warload, kg -
PERFORMANCE  
Maximum speed, km/h 211
Cruising speed, km/h 170
Range, km 602
Combat range, km
-
Service ceiling, m
6.700
Rate of climb, m/min 324
Maximum overload, g -
ARMAMENT Doesn't have (defensive).





Photos UTVA-66