The engine fitted is a Siemens seven-cylinder, radial air-cooled ol 70-80 h.p. The petrol tank is situated in the fuselage.
Type DP II two seat trainer DP IIa two seat trainer
Engine 1 Siemens Sh 4 1 Siemens Sh 5
Dimensions Length 5.90 m, height 2.50 m,  span 7.20 m, wing area 15.50 m2, aspect ratio 3. Length 5.97 m, height 2.88 m,  span 7.76 m, wing area 16.32 m2, aspect ratio 3.4
Weights Empty 340 kg, fuel 70 kg, oil 7 kg, load 220 kg,  flying weight 560 kg, wing loading 36.1 kg/m2 Empty 420 kg, fuel 70 kg, oil 7 kg, load 240 kg,  flying weight 660 kg, wing loading 40.5 kg/m2
Performance Max. speed 130 km/h, cruising speed 120 km/h, climb 2.4 m/sec, to 1000 m 7 min., service ceiling 2800 m,  range 450 km, landing speed 60 km/h Max. speed 160 km/h, cruising speed 130 km/h, climb 2.0 m/sec, to 1000 m 8 min., service ceiling 3200 m,  range 500 km, landing speed 65 km/h