Albatros D II
by last date | by total length | by number


LATEST COMMENTS

29.01.2026 04:58

Junkers Ju 390

28.01.2026 19:31

De Havilland Canada DHC-5 Buffalo

28.01.2026 02:34

25.01.2026 22:26

AAA Vision

25.01.2026 06:28

25.01.2026 03:32

Fairchild KR-34

20.01.2026 16:14

19.01.2026 03:44

18.01.2026 03:28

Convair F-102 Delta Dagger

17.01.2026 21:01

Beriev MBR-2

17.01.2026 21:01

17.01.2026 21:01

17.01.2026 21:01

17.01.2026 21:00

Aviatik (Berg) 30.14

17.01.2026 21:00

Koolhoven FK 50

17.01.2026 21:00

17.01.2026 21:00

17.01.2026 20:59

17.01.2026 20:59

17.01.2026 20:59

Bestetti-Colombo C.3

17.01.2026 20:59

17.01.2026 20:58

17.01.2026 20:57

17.01.2026 20:57

17.01.2026 20:57

17.01.2026 20:56

17.01.2026 20:56

Kawanishi H8K Emily

17.01.2026 20:55

Antonov An-71

17.01.2026 20:55

Albatros D II

17.01.2026 20:55


lxbfYeaa, e-mail, 17.01.2026 20:55

20


Klaatu83, e-mail, 29.10.2011 20:52

The principal difference between the Albatros D-I and D-II was that the D-II's top wing was lowered slightly in order to improve the pilot's view forward and upward. The modification was made at the suggestion of pilots who had flown the D-I in combat.



Fatal error: Uncaught Error: Undefined constant "isMob" in /data03/virt15346/domeenid/www.aviastar.org/htdocs/comments/comments.php:165 Stack trace: #0 {main} thrown in /data03/virt15346/domeenid/www.aviastar.org/htdocs/comments/comments.php on line 165