CICARÉ 7T - TECHNICAL SHEET
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Seating ENGINE Manuf/Model Type Maximum power WEIGHT Empty MTOW (maximum takeoff weight) PERFORMANCE Maximum speed VNE Cruising speed Vertical speed Service ceiling Fuel type Autonomy 280 Kg - 617 lbs 460 Kg - 1014 lbs 194 Km/h - 104 kt 160 Km/h - 86 kt 7 m/s - 1400 ft/min 3050 m - 10000 ft Mogas RON 95 E10 / AvGas UL91/UL94 2,5 hrs. T WO S EATS The CICARÉ 7T is a tandem seat helicopter that has come out as an option to the single seat helicopter 7B. It´s equipped with a Rotax 914UL. Approved in France as an ultralight Class 6 helicopter.

Stan d ard Compone nts of t h e CI CARÉ 7 T H e lico pte r K IT - Fuselage with SAE 4130 steel tubes. - Skates made with SAE 4130 steel tubes and aluminum. - Main gearbox with control system. - Main rotor with composite blades. - Tail rotor gearbox. - Tail rotor with composite blades. - Vertical and horizontal stabilizer made of aluminum. - Tail boom with cardan transmission and push-pull control system. - Composite cabin, including windshield, doors, engine cover, seat and seat belt. - Two fuel tanks. - Standard instrument panel. A. Engine double rotor tachometer. B. Main transmission...

S a l a d i llo, P rov i n cia d e B u e n o s Aire s , A rg e n ti n a w w w.c ica re.co m . a r s a les @ c ica re.co m . a r in