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
Design authority: Cierva Autogiro Company Ltd.
Primary manufacturer: Cierva Autogiro Company Ltd.
Parent type: Cierva Skeeter
Aircraft status: No longer flying
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)