DA20-C1 Flight Manual
General
Doc # DA202-C1 April 06, 2010 Page 1 - 12
Revision 25
CG position:
Distance from the reference datum to the CG. It is determined by dividing the
total moment (sum of the individual moments) by the total weight.
Center of Gravity Limits:
The CG range which an airplane with a given weight must be operated within.
Usable Fuel:
The amount of fuel available for the flight plan calculation.
Unusable Fuel:
The amount of fuel remaining in the tank, which cannot be safely used in flight.
Empty Weight:
Weight of the airplane including unusable fuel, all operating fluids and maximum
amount of oil.
Useful Load:
The difference between take-off weight and empty weight.
Maximum Take-off Weight:
Maximum weight permissible for take-off.
1.11.6. Equipment
ACL: Anti collision light
1.11.7. Miscellaneous
GFRP - Glass Fibre Reinforced Plastic
CFRP - Carbon Fibre Reinforced Plastic
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