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SKYLEADER UL-39 ALBI

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.

SKYLEADER UL-39 ALBI

SKYLEADER UL-39 ALBI

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  

READY TO FLY?

All of our aircraft are made-to-order based on your specifications. If you're ready to learn more about how you can add the unmatched capabilities of the UL-39 Albi to your fleet, contact your nearest dealer today!

SKYLEADER UL-39 ALBI

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