Flight Weight And Center Of Gravity; Loading Plan Diagram - Diamond DA20-C1 Manual

DA20-C1 Flight Manual
6.4.

FLIGHT WEIGHT AND CENTER OF GRAVITY

The followin g data enables the pilot to operate the DA20-C1 within the required weight and
center of gr avity limitations.
The followin g diagrams,
Figure 6.5 Loading Plan
Figure 6.6 Weight & Balance Diagram
Figure 6.7 Calculation of Loading Condition
Figure 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
Doc # DA202-C1
Revision 24
Figure 6.5. Loading Plan
April 16, 2009
Weight and Balance
be taken
identified
ent for
igu re
its of
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DOT Approved