0 MPH
TOP SPEED
0 MI
RANGE
0
HORSEPOWER
0
CAPACITY
THE FUTURE OF ULTRALIGHT AVIATION
This ultralight airplane, powered by an unconventional power plant, consisting of a reciprocating internal combustion engine driving the fan, was conceived through the cooperation of the staff and students of the Department of Aerospace Engineering at the Faculty of Mechanical Engineering of the Czech Technical University Prague, and the companies LA composite, s.r.o., and Zall JIHLAVAN airplanes, s.r.o. When completed, this completely new and thus far never implemented concept of an ultralight airplane will off er the market the properties of a jet airplane in the ultralight category, where conventional jet propulsion with hot exhaust gases is not possible, due to legal constraints.
PERFORMANCE SPECS
Never Exceed Speed (VNE)
Maneuvering Speed (VA)
Min. Speed with Flaps (VS0)
KM/H
KNOTS
MPH
SPEEDS
Cruise Speed @ 75% Power (VC)
Min. Speed without Flaps (VS1)
Engine Type
Propeller
ENGINE & PROPELLER
Maximum Power
Fuel Capacity
Range
FUEL CAPACITY & ENDURANCE
Endurance
Take-off Distance
Landing Distance
Weight
TAKE-OFF & LANDING
Take-off Run
Landing Run
Basic Empty Weight
Wing Span
Overall Height
Aspect Ratio
DIMENSIONS
Overall Length
Wing Area
Cabin Width
* All data provided in specific configuration (propeller, engine) and under ISA
GALLERY
FULL GALLERY
SKYLEADER UL-39 ALBI
EXPLORE THE