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#2852

TL Ultralight TL-32 Typhoon

🇨🇿 Czech Republic ·first flight unknown· two seat ultralight

TL Ultralight TL-32 Typhoon, photo 1 of 5
1/5 PrzemekMac· CC BY-SA 3.0

what is it?

The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s.

How to recognise it: 1 piston engine with propeller · high wing · tricycle gear · 10.7 m wingspan

base stats

  • speed 110 km/htop speed
  • range 300 kmwithout refuelling
  • size 400 kgmax take-off weight
  • built 200made in total

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

  • Wingspan of 10.7 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
—
introduced
1991
number built
200
role
two seat ultralight
origin
🇨🇿 Czech Republic
makers
TL Ultralight
engines
1× Rotax
length
5.9 m
wingspan
10.7 m
height
2.5 m
max take-off weight
400 kg
top speed
110 km/h
cruise speed
90 km/h
range
300 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 Q7670625, Wikipedia: TL Ultralight TL-32 Typhoon (CC BY-SA 4.0).Updated 2026-10-24.

stan runge 704880d source