The CICARÉ 7B (originally CH-7B) is a one seat experimental helicopter “for sport use.” It is an evolution of the CH-6 and CH-7 designs from the 1990s, manufactured by its original designer Augusto Cicaré in Saladillo, Argentina. 

Overview

Data on design, manufacture and status

Design authority: Cicaré S.A.

Primary manufacturer: Cicaré S.A.

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Single seater

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 2.48 m (8.1 ft)

Overall Length: 7.15 m (23.5 ft)

Overall Width: 6.28 m (20.6 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Rotax Rotax 912 reciprocating

Engine manufacturer: BRP-Powertrain GmbH & Co KG

Max continuous power: 100 kW (134 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 430 kg (948 lb)

Related VFS Resources

Resources related to the 7B , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the 7B , provided by public sources across the internet.

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