Development and First Flight
The A.9 was a training aircraft developed by the Italian firm Breda. Its maiden flight occurred in 1928, equipped with an Isotta-Fraschini engine producing 250 hp. Several examples of this aircraft were produced.
The A.9bis Aerobatic Variant
Subsequently, an aerobatic version, designated A.9bis, was introduced. This variant featured reduced dimensions, with a wingspan of 8.72 meters, and a lighter mass, weighing 720 kg empty and 940 kg at maximum takeoff weight.
Technical Specifications
| Modification | A.9 |
| Wingspan, m | 9.32 |
| Length, m | 7.95 |
| Wing area, m2 | 27.00 |
| Empty weight | 770 |
| Normal takeoff weight | 1050 |
| Engine type | 1 Piston engine Isotta-Fraschini |
| Power, hp | 1 x 250 |
| Maximum speed, km/h | 185 |
| Cruising speed, km/h | 152 |
| Practical range, km | 800 |
| Practical ceiling, m | 6000 |
| Crew, crew members | 2 |
Image and diagram gallery of the A.9
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How to cite this article:
APA: A.9 (). A.9. wp.archivoaereo.com. https://wp.archivoaereo.com/en/a-9-3/
VANCOUVER: A.9 [online]. wp.archivoaereo.com; [cited 2026-08-02]. Available at: https://wp.archivoaereo.com/en/a-9-3/