With the advent of the fibreglass designs onto the Australian scene during the mid 1960’s the Australian manufacturer; Edmund Schneider Ltd., began to look at a replacement for the very successful ES52 Kookaburra trainer. This resulted in the development of the ES63; a 17 metre span high performance two seater of advanced concept. A lack of capital combined with a difference of opinion with the GFA Design and Development Committee resulted in the project being shelved. In 1982 Harry Schneider revived the concept incorporating some design changes and improvements to bring the project up to date. This resulted in a prototype; the ES65 Platypus, being built and first flown on 2nd August 1984 with side by side seating.

Unfortunately the venture capital to finance the glider’s production has not been forthcoming. The prototype is of wood/glass construction. The prototype’s two piece wing is of 17 metre span, with a beech spar, birch ply skin covered by GFRP (the production wing was to be of GFRP construction). Seating is side by side arrangement in a most spacious cockpit. The two piece canopy with the aft section being rear hinged has ample visibility through large areas of perspex to the point of being able to see the rudder during flight. Rudder pedals and seats are adjustable allowing good accommodation for pilots of any size for long flights, with or without parachutes. The tail is mounted low on the fin with both rudder and elevator having horn balances smoothly blended into the design. There are three wheels on the centre line of the fuselage and, on entering the cockpit, the nose drops comfortably onto the forward wheel. This has made a reasonable balance about the main wheel possible, making the tail quite light to lift during on-ground manhandling.

The aircraft is fairly sensitive in pitch, picking up speed rapidly on lowering the nose. Thermalling requires a speed of around 50 knots, while exhibiting good stability in circling allowing for relaxed handling while thermalling. Rate of roll from 45 degrees bank to 45 degrees is 4.5 secs. The Platypus spins well, with a smooth slowish turn, not very steep from which recovery is precise and rapid with standard spin recovery procedures. The performance seems to be good for instructing cross-country flights over long distances. The side by side seating causes some initial confusion with horizon perception in turns, but the advantages are for the instructor in assessing the student, and the ability to communicate and demonstrate.

Wing span: 17.7 m
Wing area: 15.8 sq.m
Empty Weight: 400kg
Gross Weight: 590 kg
Airfoil: Wortmann FX61
L/DMax: 1:38
Seats: 2