Development and Origins
The Breguet Br.413 was a bomber-reconnaissance aircraft developed by the French firm Societé Anonyme des Atelliers d’Aviation Louis Breguet.
Features and Production
This aircraft represented a re-engined variant of the Breguet Br.410. Its maiden flight occurred in February 1933, and only four examples of this aircraft were produced in total.
Technical Specifications
| Modification | Br.413 |
| Wingspan, m | 20.20 |
| Length, m | 11.30 |
| Height, m | 5.09 |
| Wing area, m2 | 67.15 |
| Empty weight | 3500 |
| Normal takeoff weight | 7200 |
| Engine type | 2 Piston engines Hispano-Suiza 12Ybrs |
| Power, hp | 2 x 650 |
| Maximum speed, km/h | 310 |
| Cruising speed, km/h | 285 |
| Practical range, km | 1300 |
| Rate of climb, m/min | 444 |
| Service ceiling, m | 10000 |
| Crew, crew members | 4 |
| Armament | two 7.7-mm Lewis machine guns (two forward and two rear); bomb load up to 1300 kg |
Image and diagram gallery of the Breguet Br.413
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