Albatros L 69 |
| Type | Two seat trainer | a Two seat trainer |
| Engine | 1 Bristol Lucifer | 1 Siemens Sh 12 |
| Dimensions | Length 6.08 m, height 2.64 m, span 8.06 m, wingarea 10.85 m2 | Length 6.10 m, height 2.57 m, span 8.06 m, wingarea 14.00 m2 , aspect ratio 6 |
| Weights | Empty 470 kg, crew 160 kg, fuel 40 kg, flying weight 670 kg | Empty 480 kg, crew 160 kg, fuel 45 kg, flying weight 685 kg |
| Performance | Max. speed at sea level 175 km/h, climb to 1000 m 4 min., landing speed 108 km/h, range 340 km, service ceiling 4000 m | Max. speed at sea level 170 km/h, landing speed 105 km/h, endurance 2 h, climb to 500 m 2 min., to 1000 m 4 min., service ceiling 4000 m |
| Type | WerkNr. | Registration | History |
| D-684 | |||
| a | 10071 | D-778 | In Febr. 1928 registered to DVL, Adlershof. Dismantled in April 1929 |
| a | 10072 | D-1533 | Registered to the Albatros company Nov. 1928. Scrapped in Jan. 1931 |
Number built: L 69 2 L 69a 2 |
Designed by R. Schubert. Two L 69 was always at Lipezk. In 1927 Kurt Ungewitter, testpilot at the company, crashed fatally with a L 69a. The L 69 was the winner in the Sachsen-Rundfluges 1925 in class D |
