DA20-C1 Flight Manual
Supplement 4
NOTE
See example calculation of loading condition Figure 6.6. Change in center of gravity is due to
fuel consumption
Figure 6.7. Permissible Center of Gravity Range and Permissible Flight-Weight-Moment
7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
The gross weight increase to 800 kg. does not affect the description of the airplane and its
systems.
8. HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE
The gross weight increase to 800 kg. does not affect the Handling, Preventative and Corrective
Maintenance.
THIS SUPPLEMENT IS APPLICABLE ONLY TO THOSE AIRCRAFT WHICH ARE REGISTERED
IN THE UNITED STATES OR CANADA
Doc # DA202-C1 April 06, 2010 Page S4 - 16
Revision 25 DOT Approved