Type Single seat experimental glider
Dimensions Length 4 m, span 8 m, wing area 11 m2
Weights Empty 45 kg
Performance
Type Werk.Nr Registration History
Designed by E. Langer, built by the Hannoversche Waggonfabrik, A.-G in 1923
The next construction did not have a long life. From the outset called an experimental design, a wing-controlled small glider built at the  HAWA, the "Spatz". The tail end of the fuselage was a pure damping surface. To control, both wing tips were designed as a pendulum tail. For aileron, elevator and rudder control both surfaces could be moved individually. The design  seems to be diffcult in control.during flight