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

Design authority: De Havilland Aircraft Company

Primary manufacturer: De Havilland Aircraft Company

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Gyroplane

Compound type: Lift

Lift configuration: Single main rotor

Dedicated control device: Rudder

Dedicated propulsion devices: 1

Crew required: 1

Crew seating: Tandem

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Length: 10.36 m (34.0 ft)

Overall Width: 10.36 m (34.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: De Havilland Gypsy III reciprocating

Engine manufacturer: De Havilland, Engines

Take-off / rated power: 89 kW (120 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 816 kg (1799 lb)

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Related Public Resources

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

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