4 photos from Wikimedia Commons · credits & licences
- 1. Sm-2: Wisnia6522· Public domain
- 2. PZL-Swidnik SM-2 05 (6967734235): Alan Wilson· CC BY-SA 2.0
- 3. WSK SM-2: Varga Attila· CC BY-SA 3.0
- 4. SM-2 in Świdnik: MAx 92· CC BY-SA 3.0
what is it?
The PZL SM-2 was a Polish light utility helicopter, enlarged version of license-built Mil Mi-1, developed and produced by WSK PZL-Świdnik. It was also known as the WSK SM-2.
How to recognise it: 1 piston engine · 14.3 m main rotor
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 67 years ago, in 1959.
- Rotor of 14.3 m: about 3 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
- 1959-11-18
- introduced
- 1961
- retired
- 1981
- status
- retired
- number built
- 86
- role
- light utility helicopter
- origin
- 🇵🇱 Poland
- makers
- PZL-Świdnik
- engines
- 1× Lit-3 (licensed Ivchenko AI-26V)
- crew
- 1
- passengers
- 4
- length
- 17 m
- rotor diameter
- 14.3 m
- height
- 3.3 m
- max take-off weight
- 2,511 kg
- top speed
- 170 km/h
- cruise speed
- 130 km/h
- range
- 310 km
- ceiling
- 4,000 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
family
Sources: Wikidata Q688643, Wikipedia: PZL SM-2 (CC BY-SA 4.0).Updated 2026-10-24.