Breda A.1
Origins of the Breda A.1
The A.1 was a light aircraft developed by the Italian firm Breda. This aircraft marked a significant milestone, as it was the first light aircraft designed and produced by the company.
Technical Specifications and Production
Equipped with a Colombo 110 piston engine, delivering 140 horsepower, the A.1 took to the skies for its maiden flight in 1924. Several units of this pioneering aircraft were manufactured, contributing to Breda’s early aviation endeavors.
Technical Specifications
| Modification | A.1 |
| Upper wingspan, m | 10.20 |
| Aircraft length, m | 9.00 |
| Aircraft height, m | 3.20 |
| Wing area, m2 | 43.00 |
| Empty weight | 860 |
| Maximum takeoff weight | 1100 |
| Engine type | 1 Piston engine Colombo 110 |
| Power, hp | 1 x 140 |
| Maximum speed, km/h | 138 |
| Cruising speed, km/h | 110 |
| Service ceiling, m | 3000 |
| Crew, crew members | 2 |
Image and diagram gallery of the Breda A.1
 A.1 |
 A.1 |
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.