Changhe Aircraft

Manufacturer:

Changhe Aircraft

Country:

China

Commercial designation:

Z-8

Technical designation:

Z-8

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

ALL

Flight conditions:

VFR

First flight:

1999

Landing system:

wheels

Blades number:

6

Tail blades number:

5

MTOW with external loads:

12074 kg

26623.17 lbs

MTOW with only internal loading:

12074 kg

26623.17 lbs

Empty weight:

6980 kg

15390.9 lbs

External payload:

5000 kg

11025 lbs

Internal payload:

4000 kg

8820 lbs

Standard fuel tank:

3120 kg

6879.6 lbs

with optionnal external fuel tank:

4640 kg

10231.2 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

248 km/h

133.92 kt

Vne:

315 km/h

170.1 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

800 km

432 nm

Max range with auxiliary external tanks:

1400 km

756 nm

Max endurance @ min consumption speed:

04:10:00 h:min

Rate of climb @ SL:

11.5 m/s

2263.2 ft/min

Rate of climb @ SL @MTOW:

6.6 m/s

1298.88 ft/min

IGE max hovering altitude, MTOW:

5500 m

18040 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

4400 m

14432 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

6000 m

19680 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

CLXMW

Model:

WZ-6

Engines quantity:

3

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

232 km/h

125.28 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

3384 kW

4598.856 hp

Transmission shaft max continuous power:

3072 kW

4174.848 hp

Transmission shaft max power:

3072 kW

4174.848 hp

Takeoff power 5 min:

0 kW

0 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

23 m

75.44 ft

Rotor diameter:

18.9 m

61.992 ft

Tail rotor diameter:

4 m

13.12 ft

Fuselage length:

20.27 m

66.4856 ft

Overall height:

6.66 m

21.8448 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

2

Max pax number:

39

Average price:

0 $