The aircraft was intended to be a training aircraft.

Source: ”Helicopters & Autogyros of the World”, Paul Lambermont with Anthony Pirie, Second edition 1970, Cassell & Company Ltd, SBN 304 93390 2

See also the reference below for a detailed description of the aircraft.

Source: "CIerva Skeeter Flies", FLIGHT, 21st October 1948, Pages 477-478

Overview

Data on design, manufacture and status

Parent type: Cierva Skeeter

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: TBA in Side-by-side arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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