Type	S 1 Two seat trainer and sportplane	S 1a  Two seat trainer and sportplane	S 1b Two seat trainer and sportplane
Engine	1 Siemens Sh 10	1 Siemens Sh 5	1 Junkers L 1
Dimensions	Length 8.10 m, height 2.30 m, span 12.00 m, wing area 22 m2
Weights	Empty 470 kg,crew 160 kg, fuel 40 kg, flying weight 670 kg, powerload 12 kg/hp	510 kg, crew 160 kg, fuel 70 kg, flying weight 740 kg	Empty 510 kg, crew 160 kg, fuel 70 kg, flying weight 740 kg
Performance	Max. speed 130 km/h at sea level, climb to 1000 m 12 min, cruising speed 120 km/h at sea level, landing speed 50 km/h, service ceiling 3000 m, required runway for take off 125 m	Max. speed 140 km/h at sea level, climb to 1000 m 10 min, landing speed 55 km/h, service ceiling 3500 m, required runway for take off 125 m, range 350 km	Max. speed 140 km/h at sea level, climb to 1000 m 10 min, landing speed 55 km/h, service ceiling 3600 m, required runway fo take off 125 m

 

Type	WerkNr.	Registration	History
a		D-165	Sold to A. Lüber, Saulgau
	15	D-790	First Siemens Sh 10, later Sh 4. In Febr. 1928 it belonged to Luftfahrt GmbHat Halberstadt. From Febr. 1929 to K. Werner, Kaiserslautern
a	20	D-817	Sh 12 engine. In Febr. 1928 it was owned by DVL e. V., Adlershof. From April 1928 by the Albatros company and from March 1932  by H. Ryll, Berlin
		D-820	Sh 5 engine
a	22	D-853	Sh 5 engine, from March 1930 Sh 11. Owned from Jan. 1929 by the DVL e. V., Adlershof
a	23	D-866	Sh 5 engine
	27	D-966	Sh 5 engine. In april 1928 registered to DVS GmbH. From June 1928 to DVL e. V.
	21	D-994	Sh 12 engine. In Febr. 1928 owned by the Deutsche Luftfahrt GmbH. From June 1932 by  H. Jensen, Erfurt
b	29	D-1056	Belonged to DVS GmbH. From May 1929 owned by the Flugwissenschaftliche Gruppe, T.H. Braunschweig