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The prototype Potez VIII two-seat tourer/ elementary trainer was first flown on 9 April 1920, powered by a specially designed Potez engine, the 37kW Potez A 4. A light unequal-span biplane, the Potez VIII had four-wheel landing gear, the tailskid being used for landings only. The unusual A 4 engine was a complete failure and plans were made to produce 100 series aircraft
powered by the 52kW Anzani 6Ab radial. Versions built included the Potez VIII A of 1922 with the 60kW Anzani 6 A3 engine and two-wheel conventional landing gear; five were built, two of them later being converted to Potez VIII configuration and one as the Potez VIII H central-float seaplane, built especially for a wealthy Marseilles businessman.
| ENGINE | 1 x Anzani 6Ab radial piston engine, 52kW |
| WEIGHTS |
| Take-off weight | 470 kg | 1036 lb |
| Operating empty weight | 240 kg | 529 lb |
| DIMENSIONS |
| Wingspan | 8.0 m | 26 ft 3 in |
| Length | 5.72 m | 18 ft 9 in |
| Wing area | 20.0 m2 | 215.28 sq ft |
| PERFORMANCE |
| Max. speed | 142 km/h | 88 mph |
| Ceiling | 4000 m | 13100 ft |
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