Diamond Aircraft DV 20 E - 6.4 FLIGHT MASS AND CENTER OF GRAVITY

Mass and Balance DV 20 E AFM
Page 6 - 6 Rev. 2 22-Mar-2022 Doc. No. 4.01.25-E
6.4 FLIGHT MASS AND CENTER OF GRAVITY
The following information enables you to operate your DV 20 E within the permissible
mass and balance limits. For the calculation of the flight mass and the corresponding CG
position the following tables and diagrams are required:
6.4.1 - MOMENT ARMS
6.4.2 - LOADING DIAGRAM
6.4.3 - CALCULATION OF LOADING CONDITION
6.4.4 - PERMISSIBLE CENTER OF GRAVITY RANGE
The diagrams should be used as follows:
1. Take the empty mass and the empty mass moment of your airplane from the Mass
and Balance Report, and enter the figures in the appropriate boxes under the column
marked ‘Your DV 20 E' in Table 6.4.3 - CALCULATION OF LOADING CONDITION.
2. Read the fuel quantity indicators to determine the fuel quantity in the fuel tank.