Utva 66 Glider

Compare…

All gliders

Manufacturer
Utva
Description
The UTVA-66 is a STOL light utility and liaison aircraft produced in the former Yugoslavia.
ICAO Code
UT66
First Flight
1966-01-01
Designer
UTVA
Length (m)
8.38
Height (m)
3.2
Cockpit Crew
1
Max Seating
3
Max Speed (km/h)
250
Cruise Speed (km/h)
230
Min Speed (km/h)
80
Max Ceiling (m)
6700
Rate of Climb (m/s)
4.4958
Capacity Description
; 3 passengers or; 2 stretchers
National Origin
Yugoslavia
Number Built
130
Powerplant Description
1 × Lycoming GSO-480-B1J6 air-cooled flat-six engine, 201 kW (270 hp) each
Primary Users
Yugoslav Air Force
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Utva_66
Flat Wing Span (m)
11.4
Flat Wing Area (m²)
18.08
60 empty fields

Family, Model, Variant, Code Name, IATA Code, EASA TCDSN, Program Launch, Roll Out, Certification, Entry Into service, Launch Customer, Production End, Service End, Type, Category, Width, Line Logo, White Logo, One Class Typical Seating, Two Class Typical Seating, Three Class Typical Seating, Cargo Volume, Unit Load Devices, Optimum Ceiling, List Price, Armament, Endurance, Max Mach, Projected Wing Span, Projected Wing Area, Flat Wing Aspect Ratio, Projected Wing Aspect Ratio, Wing Sweepback, Wing Flattening, Max Chord, Wing boxes, Wing cells, Wing closed cells, Min Wing Load, Max Wing Load, Wing leading edge material, Wing upper surface material, Wing under surface material, Ribs material, Fuselage Diameter, Cabin Surface, Cabin Diameter, APU, Variable Cost Per Hour, Best Sink Rate, Sink Rate At Best Glide Ratio, Horizontal Speed At Best Glide Ratio, Finesse low estimation, Finesse high estimation, Finesse manufacturer value, EASA Noise Chapter, Lateral Noise Level, Flyover Noise Level, Approac hNoise Level, Cumulative Noise Level