6 photos from Wikimedia Commons · credits & licences
- 1. Changhe Z-10: Shimin Gu· GFDL 1.2
- 2. (SGP-Singapore) Aviation Industry Corporation of China Changhe Z10-ME Z10ME-02 @ Singapore Airshow 2024-02-25: S5A-0043· CC BY-SA 4.0
- 3. Changhe Z-10 helicopter armament: Z3144228· CC0
- 4. Z-10K: Alert5· CC BY-SA 4.0
- 5. Z-10K at China's Air Force Aviation Open Activity 20250921: 颐园居· CC BY-SA 4.0
- 6. Z-10K releasing flares at CCAS2023 (20230724125905): N509FZ· CC BY-SA 4.0
what is it?
The Changhe Z-10 (Chinese: 直-10; pinyin: Zhí-Shí; lit. 'helicopter-10') is a Chinese medium-weight, twin-turboshaft, attack helicopter built by the Changhe Aircraft Industries Corporation for the People's Liberation Army Ground Force Aviation. Designed by 602nd Aircraft Design Institute of Aviation Industry Corporation of China and Kamov Design Bureau, the aircraft is intended primarily for antitank warfare missions with secondary air-to-air combat capability.
How to recognise it: 2 turboshaft engines · 13 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 23 years ago, in 2003.
- Top speed is 2.3× a car on the Dutch motorway (130 km/h).
- Rotor of 13 m: about 3 cars parked nose to tail.
turboshaft: A turbine that turns a shaft, usually a helicopter rotor.
spec sheet
- first flight
- 2003-04-29
- introduced
- 2009
- status
- still flying
- number built
- —
- role
- attack helicopter
- origin
- 🇨🇳 People's Republic of China
- makers
- Changhe Aircraft Industries Corporation
- engines
- 2× WZ-9C
- crew
- 2
- length
- 14.2 m
- rotor diameter
- 13 m
- height
- 3.9 m
- max take-off weight
- 7,200 kg
- top speed
- 300 km/h
- cruise speed
- 230 km/h
- range
- —
- ceiling
- 6,400 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q1094179, Wikipedia: Changhe Z-10 (CC BY-SA 4.0).Updated 2026-10-24.