CICARÉ 7B - TECHNICAL SHEET

Product catalog summary

Overview: The document provides an estimated operational cost analysis and technical specifications for the CICARÉ 7B helicopter, a light single-seat helicopter designed for sports and recreational use. It highlights the costs associated with maintenance, insurance, and operation, as well as the helicopter's technical features and performance metrics.

Cost Analysis:

Insurance Costs: Liability insurance is estimated at USD 1,210, and aircraft insurance at USD 1,298.
Maintenance Costs: The 2000-hour engine overhaul costs USD 12.5, and the aircraft kit overhaul costs USD 36.47. Labor for 180 hours is estimated at USD 4.5.
Fuel and Lubricant Costs: Fuel consumption is estimated at USD 17.0, SWEPCO lubricant at USD 0.52, and Aeroshell lubricant at USD 0.03.
Inspection and Maintenance: Periodic inspection labor costs USD 9.34, and unscheduled maintenance costs USD 4.67.
Fixed and Operational Costs: Fixed costs per flight hour are USD 5.42, with an hourly overhaul reservation of USD 53.47. The direct operating cost per hour is USD 31.56, leading to a total operational cost per hour of USD 90.05.

Technical Specifications:

Engine: The helicopter is powered by a Rotax 912 ULS, 4-cylinder boxer engine with 100 HP.
Dimensions and Weight: The helicopter measures 3.3 x 1.6 x 1.1 meters, with a net weight of 250 kg and a gross weight of 550 kg.
Performance: Maximum speed is 194 km/h, cruising speed is 150 km/h, vertical speed is 7 m/s, and service ceiling is 3000 m. It has a fuel autonomy of 2.5 hours.
Construction: Features include a fuselage and skates made of SAE 4130 steel tubes, composite main and tail rotors, and a composite cabin with standard instruments.

Additional Information: The document notes that the cost estimates are rough and subject to change based on various factors such as maintenance, environmental conditions, and price fluctuations. The estimates are made in USD and are valid for comparison purposes only.

Catalog excerpts

Seating 1 ENGINE Manufacturer/Model Rotax 912 ULS Type 4 Cyl. boxer Maximum power 100 HP Weight Empty 265 Kg - 584 lbs MTOW (maximum takeoff weight) 430 Kg - 948 lbs PERFORMANCE Maximum speed VNE 194 Km/h - 104 kt Cruising speed 150 Km/h - 81 kt Vertical Speed 7 m/s - 1400 ft/min Service ceiling 3000 m - 9842 ft Fuel type Mogas RON 95 E10 / Autonomy FAT HE R O F U LT R ALIGH T H ELICO PT ERS The CICARÉ 7B is a light single-seat helicopter for sports and recreational use. It is an evolution of the CH-7 Angel with a notable increase in performance and safety due to the robust and reliable 100Hp...

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Stan d ard Compone nts of t h e CI CARÉ 7 B H e lico pte r K I T - 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 temperature...

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S a l a d i llo, P rov i n ci a 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

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CICARÉ 7B - TECHNICAL SHEET

CICARÉ 7B - TECHNICAL SHEET

Catalog excerpts

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