8 photos from Wikimedia Commons · credits & licences
- 1. Turner Army Airfield - Beech AT-10 Wichita in Flight: United States Army Air Forces· Public domain
- 2. Beech AT-10 Wichita USAF: Wikimedia Commons· Public domain
- 3. Beechcraft AT-10-GF in flight c1943: USAF· Public domain
- 4. Beech AT-10 (15954476307): SDASM Archives· Public domain
- 5. Beechcraft AT-10 F-409 - Freeman Field IL: United States Army Air Forces· Public domain
- 6. Beechcraft AT-10 ST338 - Stuttgart AAF AR: United States Army Air Forces· Public domain
- 7. Beechcraft AT-10 Wichita in flight c1943: USAF· Public domain
- 8. Beechcraft AT-10 Wichita on the ground c1942: USAF· Public domain
what is it?
The Beechcraft AT-10 Wichita is a twin-engined trainer aircraft designed and produced by the American aircraft manufacturer Beechcraft. Principally flown by the United States Army Air Forces (USAAF) throughout the World War II in the trainer role; over half of all USAAF pilots undertook transitional training in the AT-10. That AT-1o was developed during the early 1940s in response to a requirement issued by the United States Army Air Corps (USAAC) for a multi-engined trainer aircraft for pilots intended to operate bombers and transport aircraft.
How to recognise it: 2 piston engines with propellers · low wing · retractable tailwheel (taildragger) · 13.4 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 85 years ago, in 1941.
- Top speed is 2.5× a car on the Dutch motorway (130 km/h).
- Wingspan of 13.4 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
- 1941
- introduced
- 1942
- number built
- 2,371
- role
- military trainer aircraft
- origin
- 🇺🇸 United States
- makers
- Globe Aircraft Corporation, Beechcraft
- engines
- 2× Lycoming R-680-9
- length
- 10.5 m
- wingspan
- 13.4 m
- height
- 3.2 m
- max take-off weight
- 2,781 kg
- top speed
- 319 km/h
- cruise speed
- 270 km/h
- range
- —
- ceiling
- 5,151 m
- wings
- low wing
- landing gear
- retractable conventional landing gear
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q2893630, Wikipedia: Beechcraft AT-10 Wichita (CC BY-SA 4.0).Updated 2026-11-08.
