| Variants |
specs for Z-11, minor variations for variants
Z-11 - Base Series Designation; civilian market form.
Z-11E - Export Variant
Z-11J - Military variant
Z-11MB1 - Outfitted with alternative French-based Arriel 2B1A series turboshaft engine
Z-11ME1 - well attested variant designation, no reported particulars
Z-11W - Armed military variant for multirole use
CZ-11W - Armed light-attack platform with either Chinese or French engine; revamped over-battlefield capabilities and systems
Z-11WA - Military scout platform
Z-11WB - Armed attack-reconnaissance variant; all-new cockpit; revised weapons support and capabilities; multirole functionality
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| Dimensions: |
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| Main rotor diameter | 10.690m
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| Main rotor area | 89.8 m2 (967 sq ft)
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| Tail rotor diameter | 1.860m
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| Whole length | 13.012m
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| Height | 3.140m
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| Fuselage length | 11.240m
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| Weight and Load: |
|
| Empty weight | 1253kg
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| Max take-off weight | 2200kg
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| Normal take-off weight | 2000kg
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| Fuel capacity: 423 kg (933 lb) maximum
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| Powerplant | 1 × Liming WZ-8 turboshaft engine,
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| Power |
510 kW (680 hp) for take-off
450 kW (603 hp) max. continuous
350 kW (469 hp) cruise
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| Performance | (Normal takeoff weight, flight altitude 1000m, ISA)
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| Max Speed | 170 mph (280 kph; 150 kts)
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| Max cruising speed | 238km/h
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| Economic cruising speed | 218km/h
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| Max inclined climbing rate | 9.0m/s
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| Range | 600km / 375 miles
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| Endurance | 3.9h
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| Hovering IGE (IGE altitude 1.5m, ISA) | 3700m
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| Hovering OGE (ISA) | 2930m
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| Service ceiling | 5200m / 17,000 feet
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| Rate of climb | 10 m/s (2,000 ft/min) at sea level
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| Crew | 1
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| Capacity | 6
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