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.
VTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: TBA
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Max Gross Weight (ground): 549 kg (1210 lb)