8 photos from Wikimedia Commons · credits & licences
- 1. TL Ultralight TL-232 Condor AN1625617: Alan Lebeda· GFDL 1.2
- 2. TL-132 Condor OK-RUA-27 without doors: PrzemekMac· CC BY-SA 3.0
- 3. TL Ultralight TL-232 Condor AN1625616: Alan Lebeda· GFDL 1.2
- 4. TL TL-232 Condor, Private JP6301666: Felix Goetting· GFDL 1.2
- 5. TL Ultralight TL-232 Condor AN1347310: Felix Goetting· GFDL 1.2
- 6. TL Ultralight TL-232 Condor AN1569130: Alan Lebeda· GFDL 1.2
- 7. TL Ultralight TL-232 Condor AN1625467: Alan Lebeda· GFDL 1.2
- 8. TL Ultralight TL-232 Condor AN1841819: Alan Lebeda· GFDL 1.2
what is it?
The TL Ultralight TL-132 Condor and TL-232 Condor Plus are single engine, highwing ultralight aircraft designed and built in the Czech Republic in the mid-1990s. They remain in production in 2010.
How to recognise it: 1 piston engine with propeller · high wing · tricycle gear · 10.6 m wingspan
base stats
Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).
fun facts
- First flew 33 years ago, in 1993.
- Wingspan of 10.6 m: about 2 cars parked nose to tail.
piston: A car-like piston engine turning a propeller: simple and cheap, the classic small plane.
spec sheet
- first flight
- 1993
- number built
- 115
- role
- ultralight
- origin
- 🇨🇿 Czech Republic
- makers
- TL Ultralight
- engines
- 1× Rotax 582 UL-DCDI
- length
- 6.1 m
- wingspan
- 10.6 m
- height
- 2.3 m
- max take-off weight
- 450 kg
- top speed
- 160 km/h
- cruise speed
- 140 km/h
- range
- 450 km
- wings
- high wing
- landing gear
- tricycle gear
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q7670624, Wikipedia: TL Ultralight Condor (CC BY-SA 4.0).Updated 2026-10-24.