Type	WerkNr.	Registration	History
E/1 = E I	58		Rolls-Royce Eagle IX. To Japan
E/1 = E I	59		Rolls-Royce Eagle IX. To Chile
E/2 = E II	72	D-932	Took part in the Seeflugzeug-Wettbewerb 1926 with Jupiter engine, engine damaged by water spray. The aircraft had to be withdrawn
E/2 = E II	73	D-933	Took part in the Seeflugzeug-Wettbewerb 1926 with Jupiter engine, engine damaged by water spray. The aircraft had to be withdrawn
			Construction work started but was not finished

One was tested in 1924 by the Swiss company Ad Astra (CH 127) from 24/9 - 31/12 1924

Type	3-seated flying boat for reconnaissance (E/1)	3-seated flying boat for reconnaissance (E/2)	3-seated flying boat for reconnaissance
Engine	1 Rolls-Royce Eagle IX	1 Gnôme-Rhône Jupiter VI	1 BMW VI 5,5
Dimensions	Length 12.45 m, height 4.75 m, span 17.1 m, wing area 51.3 m2	Length 12.86 m, height 4.75 m, span 17.6 m, wing area 52.9 m2	Length 12.45 m, height 4.75 m, span 17.1 m, wing area 51.3 m2
Weights	Empty 1925 kg, flying weight 2600 kg	Empty 1925 kg, flying weight 2600 kg	Empty 1950 kg, flying weight 2600 kg
Performance	Max. speed 162 km/h at sea level, cruising speed 140 km/h, climb to 1000 m 10 min., to 3000 m 40 min., range 600 km, service ceiling 3600 m	Max. speed 174 km/h at sea level, cruising speed 145 km/h,  range 600 km, service ceiling 4000 m	Max. speed 190 km/h at sea level, cruising speed 160 km/h, landing speed 100 km/h