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#2305

Letov LK-2 Sluka

🇨🇿 Czechoslovakia ·first flew 1988· single-seat ultralight

🛩️ light / GA piston ✓ still flying
Letov LK-2 Sluka, photo 1 of 5
1/5 Balooo(cz)· CC BY-SA 3.0

what is it?

Letov LK-2 Sluka is a Czech single-seat high-wing ultralight aircraft produced by the Letov aircraft factory in 1990s and later as a kitbuilt or custom production using tools and material which remained after the closing of the factory production. Sluka is a simple, cheap and easy to fly aircraft which contributed to a rapid growth of ultralight flying organized by then established Light Aircraft Association (LAA - Letecká amatérská asociace) in the Czech Republic. Its main purpose is a local hobby flying and a flight training as a complement to twin seat elementary trainers like Letov LK-3 and ST-4 or TL-32 Typhoon.

How to recognise it: 1 piston engine with propeller · 9.2 m wingspan

base stats

  • speed 120 km/htop speed
  • range 200 kmwithout refuelling
  • size 250 kgmax take-off weight

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 38 years ago, in 1988.
  • Wingspan of 9.2 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
1988
introduced
1991
status
in production
number built
—
role
single-seat ultralight
origin
🇨🇿 Czechoslovakia
engines
1× Rotax 447 or 503
length
5.1 m
wingspan
9.2 m
height
2.5 m
max take-off weight
250 kg
top speed
120 km/h
cruise speed
70 km/h
range
200 km
ceiling
4,000 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q6533476, Wikipedia: Letov LK-2 Sluka (CC BY-SA 4.0).Updated 2026-10-24.

stan runge 704880d source