Diamond DA20-C1 - 2.8. CENTER OF GRAVITY

DA20-C1 Flight Manual Supplement 4
Doc # DA202-C1 April 16, 2009 Page S4 - 3
2.8. CENTER OF GRAVITY
Points Gross Weight Arm (aft of datum)
(lbs) (kgs) (in) (m)
A 1653 750 7.95 .202
B 1764 800 8.07 .205
C 1764 800 12.16 .309
D 1653 750 12.48 .317
WARNING
EXCEEDING THE CENTER OF GRAVITY LIMITATIONS
REDUCES THE MANOEUVRABILITY AND STABILITY OF THE
AIRPLANE.
The procedure used to determine the center of gravity is described in Chapter 6.
Revision 24 DOT Approved