Utva 66 Information & Utva 66 Links at HealthHaven.com

Utva 66
	Utva 66 Hydro
Role	Military Training Aircraft/General Aviation Aircraft
Manufacturer	Lola Utva
Designed by	Lola Utva
First flight	1966
Status	Retired
Primary user	SFR Yugoslav Air Force
Number built	130

UTVA-66 is an aircraft with four seats, which was produced in the former Yugoslavia. It is developed on former version UTVA-60 and the first flight was in the year 1966.

[edit] Description

Plane was landing on unprepared fields and its STOL characteristics contribute predkrilca are built and flap. Cockpit is equipped with a double flight commands. Move the right front and rear seats (old version) in the plane were able to accommodate two stretcher with injured people. Float instead of landing on water, the landing gear could be mounted skis. Made of 130 UTVA-66 aircraft. The last aircraft were withdrawn military service in 1999.

[edit] Variants

66-AM (air ambulance)
66H
66V
'66 Super STOL

[edit] Operators

Yugoslavia
- SFR Yugoslav Air Force

[edit] Specifications (Utva 66)

General characteristics

Crew: 1-2
Capacity: 3 passenger person capacity
Length: 7.11 m (23 ft 4 in)
Wingspan: 9.73 m (31 ft 11 in)
Height: 3.15 m (10 ft 4 in)
Empty weight: 685 kg (1,510 lb)
Useful load: 40 kg (90 lb)
Max takeoff weight: 970 kg (2,135 lb)
Powerplant: 1× Lycoming O-480-B1J6 6 cylinder flat engine, 270 hp (201 kW)

Performance

Maximum speed: 230 km/h (124 kts)
Range: 746 km (403 nm)

[edit] See also

Comparable aircraft

[edit] External links

general tharaceristics for Utva-66