Type Two seat sportplane
Engine 1 Tatra T-100
Dimensions Length 6,90 m , height  ,  span 10,0 m , wing area  13,2 m2 ,
Weights Empty 490 kg, loaded 760 kg , max. take off weight  
Performance Max.. speed 225 km/h , cruising speed  195 km/h, range 800 km, endurance  , service ceiling  4500 m , climb to 4000 m 6 min.
Type Werk.Nr Registration History
LP+BB Preliminary registration for transfer to Luftpark
The next development was the Tatra T–201, which was intended for sport purposes and was designed in November 1937. Compared to T–101, it had slightly smaller wings of increased dihedral and smaller tail surfaces; it was a high speed design. Thanks to its outstanding flying properties the T–201 won several international competitions. However, only five T-201’s were produced. Several T-201s were used by the Luftwaffe as trainers