Albatros  L 58
Type  1 + 5 seat transportplane  a  1+ 6 seat transportplane
Engine 1 Maybach Mb IVa 1 Rolls-Royce Eagle VIII
Dimensions Length 10.89 m, height 3.80 m, span 18.00 m, wing area 44.50 m2, aspect ratio 7.28 Length 10.87 m, height 3.80 m, span 18.00 m, wing area 48.0 m2, aspect ratio 6.75
Weights Empty 1370 kg, fuel 240 kg, oil 24 kg, load 880 kg, flying weight 2250 kg, wing loading 50.56 kg/m2 Empty 1370 kg, fuel 310 kg, oil 30 kg, load 880 kg, flying weight 2250 kg, wing loading 46.87 kg/m2
Performance Max. speed at sea level 150 km/h, cruising speed at sea level 135 km/h, climb 1.4 m/sec., service ceiling 3500 m, range 540 km, endurance 4.0 h Max. speed at sea level 150 km/h, cruising speed at sea level 140 km/h, climb 2.0 m/sec., service ceiling 3500 m, range 735 km, endurance 5.0 h

 

Type WerkNr. Registration History
a   D-244 Built in 1923. To Deutsche Luftreederei GmbH and to Deutsche Aero-Lloyd AG and in 1926 to Deutsche Lufthansa. Only used in 1926
a 10002 D-245  
    D-246  
    D-287 This registration probably used only for a short period. Sold to the Sovietunion
    D-292 This registration probably used only for a short period. Sold to the Sovietunion
    D-297  
a 10006 D-576 "Wolkensegler".To Deutsche Aero-Lloyd AG and in 1926 to Deutsche Lufthansa Crashed in 5th of June 1928 at Essen