;PIK 20 Prototype and initial production version. 400 kg gross weight. Retrofit of PIK-20B flap-aileron interconnect permitted under a service bulletin. Retrofit of PIK-20B enlarged water ballast bags and corresponding 450 kg gross weight permitted under a service bulletin. ;PIK 20B Refined standard class sailplane with interconnected flaps and ailerons. Gross weight increased to 450 kg. ;PIK 20E The self-launching PIK-20E is similar to the D model, but has a retractable Rotax 501 that takes 15 turns of a manual crank in the cockpit to deploy or retract. The fuselage is slightly different, with a slight sweep-back of the wings and the tailplane is larger. The modifications to turn the PIK-20 into a motorglider were designed by
Jukka Tervamäki and the prototype first flew on 2 October 1976 as the
Tervamäki JT-6 ;PIK 20E II F Designation for PIK 20Es produced by Siren S.A. in France. ==Specifications (PIK-20D) ==