| 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 |
| Type | Werk.Nr | Registration | History |
| 55 | D-1730 | Designed in 1927 as a reconnaissance floatplane , stressed for catapults. Was tested by the E-Stelle Travemünde. Flight approval withdrawn Jan. 1932. |