3 photos from Wikimedia Commons · credits & licences
what is it?
The Mitsubishi A7M Reppū (烈風, "Strong Wind") was designed as the successor to the Imperial Japanese Navy's A6M Zero, with development beginning in 1942. Performance objectives were to achieve superior speed, climb, diving, and armament over the Zero, as well as better maneuverability – all parameters that were ultimately achieved towards the end of its development in 1945. However, limitations on Japanese industry towards the end of the war prevented the A7M from ever entering mass production or being deployed for active duty, and it never saw active service.
How to recognise it: 1 piston engine with propeller · 14 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 82 years ago, in 1944.
- Top speed is 4.8× a car on the Dutch motorway (130 km/h).
- Wingspan of 14 m: about 3 cars parked nose to tail.
- Can fly 1.2× higher than Mount Everest (8,849 m).
piston: A car-like piston engine turning a propeller: simple and cheap, the classic small plane.
spec sheet
- first flight
- 1944
- retired
- 1945
- status
- retired
- number built
- 10
- role
- carrier-based fighter
- origin
- 🇯🇵 Japan
- makers
- Mitsubishi
- engines
- 1× Mitsubishi MK9C (unified :Ha-43)
- length
- 11 m
- wingspan
- 14 m
- height
- 4.3 m
- max take-off weight
- 4,720 kg
- top speed
- 628 km/h
- cruise speed
- 417 km/h
- range
- —
- ceiling
- 10,900 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q696575, Wikipedia: Mitsubishi A7M Reppū (CC BY-SA 4.0).Updated 2026-10-24.