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 |
How to cite this article:
APA: Breda A.1 (). Breda A.1. wp.archivoaereo.com. https://wp.archivoaereo.com/en/breda-a-1-2/
VANCOUVER: Breda A.1 [online]. wp.archivoaereo.com; [cited 2026-09-11]. Available at: https://wp.archivoaereo.com/en/breda-a-1-2/


