1 Siddeley Puma
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
Type 1 + 3 airliner
Engine 1 Benz Bz IV 230 hp
Dimensions Length 7,90 m, height 3,35 m, span 13,46 m, wingarea 33,15 m2
Weights Empty 1100 kg, fuel 187 kg, oil 18 kg, crew 80 kg, payload 238 kg, flying weight 1623 kg, wing load 48,95 kg/m2
Performance Max. speed 150 km/h at sea level, cruising speed 135 km/h at sea level, climb 2,8 m/sec., service ceiling 4500 m, range 600 km, endurance 4,5 h,  landing speed 80 km/h
Type Werk.Nr Registration History
6741/18
D-24
Deutsche Luftrederei GmbH, to Deutscher Aero Lloyd 6th of Febuari 1923,  from 6/1  1926 to Lufthansa, out of service 1926
5053 D-14 To Lufthansa 1926, out of service 1928
6865 D-26 To Deutscher Aero Lloyd 6/2 1923. D-26 crashed 14th of April 1923. The three passengers were killed, the pilot Karl Noack survived badly wounded
6839 D-25 DLR Destroyed by fire April 1932
417 D-66 Built 1918. DLR "Kreuzotter". to Deutscher Aero Lloyd 6/2 1923 To Lufthansa 6/1 1926 as D-68, to RVM in 1930. Siddeley Puma
D-68 DLR, to Deutscher Aero Lloyd , to Lufthansa
419 D-9, DLR 36 Taken over from DLR, to Deutsche Aero Lloyd 679 1923. Crashed 7th of October 1924. Re-registered 1923
439
D-74 Built 1918 "Viper". DLR.  To Deutscher Aero Lloyd 6/2 1923. Taken over by the Lufthansa 6/1  1926, Siddeley PumaChristened "Viper". The aircraft crashed 14th of June 1928 in unknown circumstances in Frankfurt, killing all five occupants.
D-150 DLR. Crashed  July 1922
D-151 DLR, To Deutscher Aero Lloyd 6/2 1923, to Adria Aero Lloyd March 1925 as D-151
D-124 To Deutscher Aero Lloyd 6/2 1923, to Adria Aero Lloyd March 1925 as D-124