Robin DR400/120D - Page 102

Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 6 - 4 Issue 3 - July 2014
kg (lb)
980 (2161)
910 (2006)
720 (1587)
0.205
(8)
12
0.410
(16.16)
24
0.428
(16.85)
25
0.564
(22.2)
33
m
(in)
% of mac
Cat. N
Cat. U
Figure 6-2 Use of Weight and Balance Diagram
▲ WARNING: For the calculation of the aircraft center of gravity, do not
use the values of empty aircraft weight and moment
indicated in the above example!
Use the values indicated in the latest licensed weight
and balance data sheet of your aircraft