Type a Two seat reconnaissance aircraft b Two seat reconnaissance aircraft
Engine 1 BMW  VI 1 Siemens Jupiter VI
Dimensions Length 9,90 m , height  ,  span upper 11,5 m ,lower 10,0 m, wing area  34,57 m2 , Length 9,81 m , height  , span upper 11,5 m ,lower 10,0 m , wing area  34,57 m2 ,
Weights Empty 1780 kg, loaded 2570 kg , max. take off weight   , fuel 550 l Empty 1700 kg, loaded 2436 kg , max. take off weight   , fuel 550 l
Performance Max.. speed 240 km/h at sea level, cruising speed 220 km/h at sea level , landing speed 95km/h, range 1070 km , endurance  , service ceiling  5000 m , climb to 1000 m 2,8 min., to 2000 m 6,8 min., to 3000 m 14,8 min. Max.. speed 232 km/h at sea level, cruising speed 210 km/h at sea level  , range 1020 km , endurance  , service ceiling  5000 m , climb to 1000 m 3,2 min., to 2000 m 7,8 min., to 3000 m 16,2 min.
Type Werk.Nr Registration History
a 321 D-1694, D-IDYM Delivered to Albatros-Erpobungsabteilung July 1029. Tested at Lipezk summer 1930 with Mag  6W 12/IIIa bombmagazine and Goertz- Richtfernrohr Fl.218 (220)
b 342 D-1795, D-IXAZ To RDL Erprobungsstelle Staaken. Tested with Sh 20, SAM 22 C and SAM 322
c = HD 45a 363 D-1011, D-IBEZ See HD 45
c = HD 45a 364 D-2064, D-ILEU See HD 45
The Heinkel HD 41 was a reconnaissance aircraft developed in Germany in the 1920s.
The HD 41a, equipped with a BMW VI , paid particular attention to the flight characteristics of the aircraft, so as to add, if necessary, the machine guns to transform the apparatus into a fighter.