DA20-C1 Flight Manual
Limitations
Doc # DA202-C1 April 16, 2009 Page 2 - 6
Revision 24 DOT Approved
2.7. WEIGHT
Maximum Ramp Weight : 1660 (753 kg)
Maximum Take-Off Weight : 1653 lbs (750 kg)
Maximum Landing Weight : 1653 lbs (750 kg)
Maximum permissible weight : 44 lbs (20 kg) only permissible
in the baggage compartment with baggage harness
WARNING
EXCEEDING WEIGHT LIMITATIONS MAY LEAD TO
OVERLOADING OF THE AIRPLANE AND CAUSE LOSS OF
CONTROL OF THE AIRPLANE AND/OR STRUCTURAL
DAMAGE.
2.8. CENTER OF GRAVITY
The reference datum (RD) for the center of gravity (CG) calculation is tangent to the leading
edge of the wing at the root rib. This plane is vertical when the fuselage is horizontal.
Procedures for horizontal alignment, as well as particulars with regard to the empty weight
center of gravity, refer to Chapter 6.
Most forward CG (all weights) : 7.96 in (202 mm) aft of RD.
Most rearward CG (all weights) : 12.49 in (317 mm) aft of RD.
WARNING
EXCEEDING THE CENTER OF GRAVITY LIMITATIONS
REDUCES THE MANEUVERABILITY AND STABILITY OF THE
AIRPLANE.
The procedure used to determine the center of gravity is described in Chapter 6.
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