The Albatros L.101 was a two-seat, strut-braced high-wing monoplane used as a training and touring aircraft of mixed construction, designed by the Albatros company and produced after its takeover by Focke-Wulf-Flugzeugbau in 1932-33. The prototype took part in the 1930 Challenge competition but did not complete the technical events. A total of 71 serial aircraft were produced, which served for training at the German Air Transport Pilot School. The exhibited example bore serial number 245 and registration marks D-EKYQ.
| Wingspan | 12,35 m |
| Length | 8,45 m |
| Takeoff weight | 830 kg |
| Maximum speed | 172 km/h |
| Ceiling | 4200 m |
| Range | 660 km |
| Armament | – |
| Engine | 4-cylinder inverted inline Argus As-8A, 120 hp (89 kW) |
