Type Two seat sportplane
Engine 1 Tatra T-100
Dimensions Length  6,62 m, height 2,15 m ,  span 13,0 m , wing area  16,40 m2 ,
Weights Empty 500 kg, loaded 780 kg , max. take off weight  1100 kg
Performance Max.. speed 215 km/h , cruising speed  190 km/h,ferry  range 4500 km, practical range 1200 km endurance  , service ceiling  4500 m , climb
Armament
Type Werk.Nr Registration History
The first Tatra aeroplane of original design was a very powerful low wing monoplane with two seats in tandem. This was the experimental Tatra T–001, which had some parts in common with the Bü–131. The prototype was built and test flown through the first half of 1937, and received the registration OK–TAN. The aeroplane was very efficient and its potential for development was obvious from the outset.

The first development of the Tatra T-001 was the Tatra T–101, registered as OK–TAO. This design was characterized by the greater span of its wings and increased wing-area, which enabled the aeroplane to carry higher loads. This would prove very useful for distance flights. The tail surfaces were also somewhat enlarged. The aeroplane was designed primarily for air tourism and high performance flying, and it would soon go on to gain a number of records.