BH-10
In 1924, the Avia company created the single-seat training aircraft BH-10, based on the BH-9 model. This aircraft was specifically designed for aerobatic performances and advanced training missions.
Origin and Purpose
The prototype’s maiden flight occurred on January 3, 1924, marking the beginning of its production. Its single-seat configuration and agility made it ideal for pilot training in complex maneuvers.
Production and Service
A total of 21 units of this machine were built. Of these, 10 aircraft were supplied to the Czech Air Force, where they were designated B.10, significantly contributing to the nation’s air capabilities.
Technical Specifications
| Modification | BH-10 |
| Wingspan, m | 8.80 |
| Length, m | 5.42 |
| Height, m | 2.54 |
| Wing area, m2 | 9.80 |
| Empty weight | 288 |
| Normal takeoff weight | 414 |
| Engine type | 1 Piston engine Walter NZ-60 |
| Power, hp | 1 x 60 |
| Maximum speed, km/h | 160 |
| Cruising speed, km/h | 130 |
| Practical range, km | 480 |
| Rate of climb, m/min | 200 |
| Service ceiling, m | 4500 |
| Crew | 1 |
Image and diagram gallery of the BH-10
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Fuentes y Rigurosidad
La información presentada en esta ficha técnica ha sido compilada a partir de manuales de vuelo desclasificados, archivos históricos y bibliografía especializada. Aunque nos esforzamos por mantener la máxima precisión, algunos datos de rendimiento pueden variar según la variante específica o las condiciones operativas.