Dornier Do P
Type WerkNr. Registration History
    CH 302 First flight 31/3 1930 at Löwenthal. Tested in Switzerland the same year, modified to a bomber at Altenrhein. In March 1931 taken over by the RVM and used as a transport. Tested at Lipezk in summer 1932. After closing down the Lipezk in October 1933 the aircraft was given to the Sovietunion.(Roeder ). Crashed during testing (Stützer )
  180 D-1982 Unarmed , used as a trainer at least until 1935

 

Type 6 seat bomber
Engine 4 Siemens Jupiter VI 6,3 u with 4-bladed wooden Dornier propellers
Dimensions Length 23.4 m, height 7.3 m, span 30.0 m, wing area 152.6 m2
Weights Empty 8000 kg, flying weight 12000 kg
Performance Max. speed 210 km/h at sea level, climb to 2000 m 13.2 min., service ceiling 3500 m, range 1000 km
Armament (Proposed, partly tested) 1 MG 15 in the nose, 1 MG 15 in a dorsal position, 1 MG 15 in the tail, 1 MG 15 in a ventral position. Bombload : 60 x 50 kg internally or 4 x 250 kg bombs externally and 20 x 25 kg bommbs internally