Harbin Aircraft

Manufacturer:

Harbin Aircraft

Country:

China

Commercial designation:

Haitun

Technical designation:

Z-9

Version, Variant:

A

Type:

fenestron

Currently produced:

Y

Typical missions:

Military

Flight conditions:

First flight:

0

Landing system:

wheels

Blades number:

4

Tail blades number:

13

MTOW with external loads:

4100 kg

9040.5 lbs

MTOW with only internal loading:

4100 kg

9040.5 lbs

Empty weight:

2050 kg

4520.25 lbs

External payload:

1600 kg

3528 lbs

Internal payload:

2038 kg

4493.79 lbs

Standard fuel tank:

926 kg

2041.83 lbs

with optionnal external fuel tank:

1070 kg

2359.35 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

280 km/h

151.2 kt

Vne:

315 km/h

170.1 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

860 km

464.4 nm

Max range with auxiliary external tanks:

1000 km

540 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

6.6 m/s

1298.88 ft/min

IGE max hovering altitude, MTOW:

2150 m

7052 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:

1150 m

3772 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:

4570 m

14989.6 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:

SAEC

Model:

WZ8A

Engines quantity:

2

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:

0 km/h

0 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:

1052 kW

1429.668 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 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:

13.68 m

44.8704 ft

Rotor diameter:

11.93 m

39.1304 ft

Tail rotor diameter:

1.1 m

3.608 ft

Fuselage length:

0 m

0 ft

Overall height:

3.97 m

13.0216 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:

12

Average price:

0 $