


| Type | Two seat reconnaissance aircraft |
| Engine | 1 Siemens Jupiter VI |
| Dimensions | Length , height , span , wing area , |
| Weights | Empty , loaded , max. take off weight |
| Performance | Max. speed 265 km/h endurance 3 h range 600 km |
| Type | Werk.Nr | Registration | History |
| 98 | D-1708, D-IQIM | Tested at Lipetsk 1932. To Rechlin 1937 Modified to Fw 39B Damaged during training flight, scrapped |