CICARÉ 8R - TECHNICAL SHEET

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CICARÉ 8R - TECHNICAL SHEET

Product catalog summary

Estimated Operational Costs:

Insurance Costs: Liability insurance is estimated at USD 1,562 and aircraft insurance at USD 1,650.
Maintenance Costs: The 1200-hour engine overhaul is USD 37.37, and the 2000-hour aircraft kit overhaul is USD 53.8. Labor costs for 180 hours at USD 50 per hour total USD 4.5.
Fuel and Lubricant Costs: Fuel consumption is 22 liters per hour at USD 1.0 per liter, totaling USD 22.0. SWEPCO lubricant costs USD 0.86, and Aeroshell lubricant costs USD 0.06.
Inspection and Maintenance: Periodic inspection labor costs USD 9.34, and unscheduled maintenance costs USD 4.67.
Fixed and Direct Costs: Fixed cost per flight hour is USD 6.42, with an hourly overhaul reservation of USD 95.67. Direct operating cost per hour is USD 36.93, leading to a total operational cost per hour of USD 139.02.

Technical Specifications:

Engine: Rotax 915 iS, 4 Cylinder boxer, with a maximum power of 141HP and continuous power of 135HP.
Weight: Empty weight is 330Kg (730 lb), and MTOW is 525Kg (1160 lb).
Performance: Maximum speed is 194 Km/h (100kt), cruising speed is 148 Km/h (80kt), vertical speed is 10 m/s (2000 ft/min), hover ceiling is 1830 m (6000 ft), and service ceiling is 3050 m (10000 ft).
Fuel Type: Mogas RON 95 E10 / AvGas UL91/UL94.
Autonomy: 2.7 hours with seating for 2 (side by side).

Design and Features:

The helicopter is described as maneuverable and efficient, with a semi-rigid engine allowing sharp maneuvers and low vibrations. It boasts a 30% lower fuel consumption compared to similar certified helicopters.
Standard components include a fuselage made of SAE 4130 steel tubes, composite material rotor blades, and a comprehensive set of manuals and tools for maintenance.

Dimensions:

Length x Height x Width: 3.3 x 1.6 x 1.6m.
Net weight: 250kg, Gross weight: 550kg.

Additional Information:

The document notes that the cost estimates are rough and subject to change based on various factors such as use, maintenance, and environmental conditions. Prices are in USD and valid for comparison purposes only.

Catalog excerpts

DATA SH E E T Seating ENGINE Manufacturer/Model Type Maximum power Maximum continuous power WEIGHT Empty MTOW (Maximum takeoff weight) PERFORMANCE Maximum speed VNE Cruising speed Vertical speed (MTOW) Hover ceiling (MTOW) Service ceiling FUEL TYPE AUTONOMY 2 (side by side) Rotax 915 iS 4 Cylinder boxer 141HP 135HP B EST P OWE R-WE I GH T RAT IO IN ITS CLASS Maneuverable and efﬁcient. An extremely agile helicopter. Its semi-rigid engine allows sharp maneuvers with very low vibrations, even at maximum power.The cutting-edge engineering and design team produced a helicopter with aimpressive unprecedented...

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Stan d ard Compone nts of t h e CI CARÉ 8 H e lico pte r K I T - Fuselage in SAE 4130 steel tubes. Skate system in SAE 4130 steel and aluminum tubes. Main transmission box with command systems. Main rotor with blades made of composite materials. Tail rotor transmission box. Tail rotor with blades made of composite materials. T-shaped stabilizer. Tail boom with cardan transmission and command system. Composite materials cabin. Includes windshield, doors, hood, seats and safety belts. - Object holder under the co-pilot seat - Fuel tanks -Governor. - Assembly manual. - Maintenance manual. - Parts...

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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 8R - TECHNICAL SHEET

CICARÉ 8R - TECHNICAL SHEET

Catalog excerpts

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