Developed in 1931, the C.24 is equipped with a Cierva C.19 IV three-blade rotor with tricycle landing gear.

Overview

Data on design, manufacture and status

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Gyroplane

Compound type: N/A compounded with 1 propulsors

Lift devices: 1 Single main rotor

Dedicated control device: 1 Rudder

Crew required: 1 in Tandem arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

Resources related to the C.24 , provided by the Vertical Flight Society.
Forum Proceedings
 
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Related Public Resources

Resources related to the C.24 , provided by public sources across the internet.

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