Diamond DA20-C1 - 6.4. FLIGHT WEIGHT AND CENTER OF GRAVITY

DA20-C1 Flight Manual Weight and Balance
Doc # DA202-C1 April 16, 2009 Page 6 - 8
Revision 24 DOT Approved
6.4. FLIGHT WEIGHT AND CENTER OF GRAVITY
The followin
center of gr
The followin
Figure 6.5
Figure
Figure
Figure
be taken
identified
ent
igu
its
g data enables the pilot to operate the DA20-C1 within the required weight and
avity limitations.
g diagrams,
Loading Plan
6.6 Weight & Balance Diagram
6.7 Calculation of Loading Condition
6.8 Permissible Center of Gravity Range
and permissible Flight-Weight-Moment
are to be used for calculations of the flight-weight and the center of gravity as follows:
1. The empty weight and the empty-weight-moment of the airplane should
from the weighing report or from the weight & balance report and entered into the
form "Calculation of Loading Condition" (see Figure 6.7) in the columns
with "Your DA20-C1".
2. Using the Weight & Balance Diagram (see Figure 6.6) determine the mom
each part to be loaded, and enter it in the respective column in Figure 6.7.
3. Add the weights and the moments of each column (point 4 and point 6 in F
6.7) and enter the sum in Figure 6.8 "Permissible CG Range and Permissible
Flight-Weight-Moment" to check if the values are within the permissible lim
the loading range.
4. Figure 6.5 Loading Plan
Figure 6.5. Loading Plan
for
re
of