7 photos from Wikimedia Commons · credits & licences
- 1. UT-2-1978: Leo Medvedev/Лев Леонидович Медведев· CC BY-SA 4.0
- 2. UT 2 w Szkole Orlat w Deblinie: K. Kobrzyński, K. Koszewski, T. Malinowski, J. Malujdy, ze zbiorów (from collection of): Komisja Historyczna Rady Seniorów Aeroklubu PRL, Muzeum Lotnictwa i Astronautyki w Krakowie, Ośrodek Postępu Te· Public domain
- 3. Yakovlev UT-2 Yakovlev UT-2 Yakovlev Museum Moscow Sep93 1 (17125610506): San Diego Air & Space Museum Archives· Public domain
- 4. Yakovlev UT-2 Yakovlev UT-2 Yakovlev Museum Moscow Sep93 3 (16944166937): San Diego Air & Space Museum Archives· Public domain
- 5. Yakovlev UT-2 Yakovlev UT-2 Yakovlev Museum Moscow Sep932 (17125607616): San Diego Air & Space Museum Archives· Public domain
- 6. Yakovlev UT-2, Russia - Air Force AN1359366: parfaits· CC BY-SA 3.0
- 7. Yakovlev UT-2, Russia - Air Force AN1480394: parfaits· CC BY-SA 3.0
what is it?
The Yakovlev UT-2 (Russian: Яковлев УТ-2; NATO reporting name "Mink") is a single-engine tandem two-seat low-wing monoplane that was the standard Soviet trainer during World War II. It was used by the Soviet Air Force from 1937 until replaced by the Yakovlev Yak-18 during the 1950s.
How to recognise it: 1 piston engine with propeller · low wing · 10.2 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 91 years ago, in 1935.
- Top speed is 1.6× a car on the Dutch motorway (130 km/h).
- Wingspan of 10.2 m: about 2 cars parked nose to tail.
- Range of 1,130 km: 6× Amsterdam to Brussels.
piston: A car-like piston engine turning a propeller: simple and cheap, the classic small plane.
spec sheet
- first flight
- 1935-07-11
- introduced
- 1936
- status
- retired
- number built
- 7,243
- role
- trainer
- origin
- 🇷🇺 Soviet Union
- makers
- Yakovlev, Progress (aviation plant, Arseniev)
- engines
- 1× Shvetsov M-11D / Shvetsov M-11
- crew
- 2
- length
- 7.2 m
- wingspan
- 10.2 m
- height
- 3 m
- max take-off weight
- 940 kg
- top speed
- 210 km/h
- cruise speed
- 99 km/h
- range
- 1,130 km
- ceiling
- 5,000 m
- wings
- low wing
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q932105, Wikipedia: Yakovlev UT-2 (CC BY-SA 4.0).Updated 2026-10-24.