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| CREW | 2 |
| ENGINE | 1 x 50 or 80hp Gnome, 60 or 80hp Le Rhone or 100hp Gnome Monosoupape engine |
| WEIGHTS |
| Take-off weight | 756 kg | 1667 lb |
| Empty weight | 440 kg | 970 lb |
| DIMENSIONS |
| Wingspan | 11.48 m | 38 ft 8 in |
| Length | 8.92 m | 29 ft 3 in |
| Wing area | 41.81 m2 | 450.04 sq ft |
| PERFORMANCE |
| Max. speed | 121 km/h | 75 mph |
 | A three-view drawing (800 x 659) |
| Barry, 10.11.2015 Another Henri Coanda design the TB8 was used by both the RFC and the RNAS. Shortly after the start of W.W.I. the RFC transferred all their TB8's to the RNAS. A total of 58 were built with six being exported to Romania for service with the Royal Rumanian Air Force. |
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