Diamond Aircraft DV 20 E - Calculation of Loading Condition

DV 20 E AFM Mass and Balance
Doc. No. 4.01.25-E Rev. 2 22-Mar-2022 Page 6 - 11
CALCULATION OF
LOADING CONDITION
DV 20 E
(Example)
Your DV 20 E
Mass
[kg]
[lb]
Moment
[kgm]
[in.lb]
Mass
[kg]
[lb]
Moment
[kgm]
[in.lb]
1. Empty mass (from Mass and
Balance Report)
523
1152
144.7
12559
2. Pilot and Copilot seat
Lever arm: 0.14 m (5.6 in)
163
359
22.8
2010
3. Baggage
Lever arm: 0.82 m (32.4 in)
0
0
0
0
4. Total mass & total moment
with empty fuel tank
(Total of 1.-3.)
686
1512
167.5
14569
5. Usable fuel
(0.72 kg/liter)
(6.01 lb/US gal)
Lever arm: 0.82 m (32.4 in)
42
93
34.4
3013
6. Total mass & total moment
with fuel
(Total of 4. and 5.)
728
1605
201.9
17582
The CGs shown in the following diagrams are those from the example in Section
6.4.3 - CALCULATION OF LOADING CONDITION, rows 4 and 6.