| Type |
Two seat reconnaissance floatplane |
| Engine |
1 Gnôme-Rhône Jupiter VI 9 ak |
| Dimensions |
Length 11.87 m, height 4.97 m, span 12.35 m, wingarea
49.8 m2 |
| Weights |
Empty 2402 kg, flying weight 2985 kg, crew 160 kg, fuel and
oil 350 kg, armament 73 kg |
| Performance |
Max. speed 204 km/h, climb 5 min to 1000 m, cruising speed
190 km/h at sea level, landing speed 92 km/h, range 600 km, service ceiling
5000 m, starting length 215 m |
| Armament |
Planned: 1 fixed MG for the pilot , 1 movable in a dorsal
position for the observer |
