Breda A.8
The A.8 was a night bomber developed by the Italian firm Breda. This aircraft served as an improved modification of the Breda A.3 night bomber, which had been released in 1924. Its design aimed to enhance operational capabilities for nocturnal missions.
Development and Initial Features
The aircraft’s maiden flight, initially equipped with two 400 hp Lorraine engines, occurred in 1927. These engines were soon replaced with two more powerful 500 hp Asso units, in an effort to boost performance.
Testing and Fate
However, tests of the aircraft revealed a number of shortcomings and only mediocre flight characteristics. Consequently, only a single prototype of the A.8 was ever produced, marking the end of its development.
Technical Specifications
| Modification | A. 8 |
| Wingspan, m | 23. 00 |
| Length, m | 16.70 |
| Wing area, m2 | 143.00 |
| Empty weight | 3800 |
| Normal takeoff weight | 5600 |
| Engine type | 2 Piston engines Isotta-Fraschini Asso |
| Power, hp | 2 x 500 |
| Maximum speed, km/h | 175 |
| Cruising speed, km/h | 140 |
| Practical range, km | 480 |
| Service ceiling, m | 3500 |
| Crew | 3 |
| Armament | three 7.7 mm machine guns |
Image and diagram gallery of the Breda A.8
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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.