A.10
Development and Origins
The A.10 was a training aircraft developed by the Italian firm Breda. This aircraft represented a further evolution of the existing Breda A.9 training aircraft.
Maiden Flight and Technical Specifications
Its maiden flight, featuring a powerful 250 hp Isotta-Fraschini engine, took place in 1928. In terms of characteristics, it served as an intermediate aircraft between the A.9 and A.9bis modifications.
Production
Several units of this training aircraft model were produced during its manufacturing period.
Technical Specifications
| Modification | A.10 |
| Wingspan, m | 8.84 |
| Length, m | 8.10 |
| Wing area, m2 | 17.50 |
| Empty weight | 800 |
| Normal takeoff weight | 1050 |
| Engine type | 1 Piston engine Isotta-Fraschini |
| Power, hp | 1 x 250 |
| Maximum speed, km/h | 210 |
| Cruising speed, km/h | 170 |
| Practical range, km | 800 |
| Practical ceiling, m | 5000 |
| Crew, crew members | 2 |
Image and diagram gallery of the A.10
 A.10 |
 A.10 |
ArchivoAéreo Editorial Team
A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.
Sources & Accuracy
The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.