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Cicaré CH-12
 
 Cicare-CH12-01
 
The Cicaré CH-12 side by side seat helicopter is built in the Argentne Republic, for private and recreational use. This particular design seems to incorporate the traditional style of helicopter swash plate along with a new composite cabin and tail boom.
 
 Cicare-CH12-02
 
It is equipped with a Subaru EJ25 engine, however it has been designed to also accept a Lycoming O-360.The airframe is made of SAE 4130 steel tubes. The skids are made of SAE 4130 steel tubes and aluminium.
 
The main and tail rotors are with composite blades. The vertical and horizontal stabilizer are aluminium and the cabin is composite. Dual controls are standard and two fuel tanks are fitted.
 
 Cicare-CH12-03
 
CH-12
Engine: Subaru EJ25 or Lycoming HIO-360- G1A
Rotor diam: 7,70m
Height: 2,71m
Width: 2,20m
MTOW: 700 Kg (1540 lbs)
Empty Weight: 430 Kg (946 lbs)
Maximum Speed (VNE): 205 Kmh (128 mph)
Cruise Speed: 160 kph (100 mph)
Climb Rate: 7 m/s (1380 ft/m)
Service Ceiling: 3500 m (11,500 ft)
Endurance: 3.0 hr
Seats: 2
Fuel: AVGAS 100LL
 
 Cicare-CH12-04
 
 
 
 


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