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TL UltralightOther aircraft · Fixed-wing · Czech Republic

Condor

Seats
2 2
Power
65 hp48 kW
Cruise
76 kt140 km/h
First flight
1993 1993
TL Ultralight Condor
Photo: PrzemekMac · CC BY-SA 3.0

About the Condor

The Tl Ultralight Condor is a single-engine, high-wing fixed-wing aircraft originating from the Czech Republic, designed to suit recreational pilots seeking a two-seat side-by-side layout with dual controls. It utilizes a fabric-covered metal structure with a conventional configuration, V-shaped main wing struts, and a swept fin and rudder.

Developed in the 1990s as a family of closely related ultralight models, the initial version completed its first flight in 1993, followed by an upgraded variant a year later. Production continued strongly into the following decade, with over one hundred examples successfully completed and distributed across various European and international civil registries.

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