Cicare

Manufacturer:

Cicare

Country:

Argentina

Commercial designation:

CH-12

Technical designation:

CH-12

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil

Flight conditions:

VFR

First flight:

2001

Landing system:

skids

Blades number:

2

Tail blades number:

2

MTOW with external loads:

700 kg

1543.5 lbs

MTOW with only internal loading:

700 kg

1543.5 lbs

Empty weight:

430 kg

948.15 lbs

External payload:

0 kg

0 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

0 kg

0 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

165 km/h

89.1 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

205 km/h

110.7 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

0 km

0 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

02:30:00 h:min

Rate of climb @ SL:

7 m/s

1377.6 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

0 m

0 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:

0 m

0 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:

3500 m

11480 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:

N

Engine manufacturer:

Lycoming

Model:

HIO-360-G1A

Engines quantity:

1

Powerplant category:

piston

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:

134 kW

182.106 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:

8.66 m

28.4048 ft

Rotor diameter:

7.7 m

25.256 ft

Tail rotor diameter:

1.1 m

3.608 ft

Fuselage length:

6.36 m

20.8608 ft

Overall height:

2.71 m

8.8888 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:

1

Max pax number:

1

Average price:

0 $