该AN-32型克莱恩是AN-24型焦炭的直接开发。的克莱因的主要识别差别是发动机安装在机翼，和一个大腹翅片尾段下方。翼是高位安装和从发动机到钝顶同样锥形的。Two turboprops mounted in pods over the wings which extend beyond the wings� leading and trailing edges. The fuselage is long and tubular, with upswept rear section and solid, rounded nose and stepped cockpit. The fin is unequally tapered with blunt tip and angular fairing. Flats are high-mounted on the body, back-tapered with blunt tips, and have a positive slant.
