Flight manual
MD3
RIDER
Page 6-5
Permitted range for empty weight:
270 – 304 kg
Note: different weight limit might apply due to national regulation
Center of gravity position of the empty aircraft is calculated as follows:
[ ]
[ ]
%
100
*
1152
*
)
(
*
1
1
2
2
2
L
T
P
L
L
X
X
mm
M
R
X
R
R
X
X
=
−
+
=
Permitted center of gravity range for empty aircraft:
20 – 23 %
Weightening must be performed and recorded when any change to the
aircraft configuration is made:
Center of gravity
Date:
Empty
weight M
[kg]
X
L ,
[mm]
X
T
[%]
Performed
by and date
6.2. Weight and center of gravity determination for flight
The correct center of gravity position is ensured when weight of
passengers, baggage and fuel is within the approved range (all limits
are described in section 2 of this manual)
