CICARÉ 7T - TECHNICAL SHEET

Product catalog summary

Overview: The document provides a detailed cost estimation and technical specifications for the CICARÉ 7T helicopter, a tandem seat ultralight helicopter equipped with a Rotax 914UL engine.

Cost Estimation:

Liability insurance: USD 1,265
Aircraft insurance: USD 1,375
2000 Hour Engine Overhaul: USD 19.85
2000 hour aircraft kit overhaul: USD 36.47
Labor (180 hours at USD 50/hour): USD 4.5
Fuel cost (19 l/h at USD 1.0/liter): USD 19.0
SWEPCO lubricant (2.73 liters at USD 378.0/liter): USD 0.52
Aeroshell lubricant (4.3 liters at USD 15.85/liter): USD 0.03
Periodic inspection labor: USD 9.34
Unscheduled maintenance: USD 4.67
Fixed cost per flight hour (based on 500 flight hours/year): USD 5.28
Hourly Overhaul Reservation: USD 60.82
Direct operating cost per hour: USD 33.56
Total operational cost per hour: USD 99.65

Note: Costs are estimates and may vary based on usage, maintenance, environmental conditions, and prices. Transportation costs and local taxes are not included.

Technical Specifications:

Engine: Rotax 914 UL, 4 Cyl. boxer, 115 HP
Weight: Empty - 280 Kg (617 lbs), MTOW - 460 Kg (1014 lbs)
Performance: Maximum speed - 194 Km/h (104 kt), Cruising speed - 160 Km/h (86 kt), Vertical speed - 7 m/s (1400 ft/min), Service ceiling - 3050 m (10000 ft)
Fuel type: Mogas RON 95 E10 / AvGas UL91/UL94
Autonomy: 2.5 hours
Seating: 2 seats

Standard Components:

Fuselage and skates made with SAE 4130 steel tubes and aluminum
Main gearbox and rotor with composite blades
Tail rotor gearbox and blades
Vertical and horizontal stabilizer made of aluminum
Composite cabin with standard instrument panel
Includes manuals and transport wheels

Additional Information: The CICARÉ 7T is approved in France as an ultralight Class 6 helicopter. The document also provides contact information for further inquiries.

Catalog excerpts

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.

Open the catalog to page 3

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 temperature...

Open the catalog to page 4

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

Open the catalog to page 5

CICARÉ 7T - TECHNICAL SHEET

CICARÉ 7T - TECHNICAL SHEET

Catalog excerpts

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