Diamond DA 62 - Calculation of Loading Condition

DA 62 AFM Mass and Balance
CALCULATION OF
LOADING CONDITION
DA 62
(Example)
Your DA 62
Mass
[kg]
[lb]
Moment
[kgm]
[in.lb]
Mass
[kg]
[lb]
Moment
[kgm]
[in.lb]
1. Empty mass (from Mass
and Balance Report)
1600
3528
3885.0
337,203
2. Front seats
Lever arm: 2.30 m (90.6 in)
160
353
368.0
31,941
3. Passenger seats row I
Lever arm: 3.25 m (128.0 in)
140
308
455.0
39,492
4. Passenger seats row II
Lever arm: 4.15 m (163.4 in)
60
132
249.0
21,612
5. LH Nose baggage compt.
Lever arm: 0.47 m (18.5 in)
30
66
14.1
1,224
6. RH Nose baggage compt.
Lever arm: 0.05 m (2.0 in)
30
66
1.5
130
7. Rear baggage compt.
(Section A)
Lever arm: 4.06 m (159.8 in)
0
0
0.0
0
8. Rear baggage compt.
(Sections B, C, D, F)
Lever arm: 4.18 m (164.5 in)
0
0
0.0
0
9. Rear baggage compt.
(Section E )
Lever arm: 4.41 m (173.6 in)
5
11
22.05
1,914
10. De-Icing fluid
(1.1 kg/L (9.02 lb/US gal))
Lever arm: 0.90 m (35.4 in)
10
22
9.0
781
11. Total mass & total moment
with empty fuel tanks
(Total of 1.-10.)
2035
4486
5003.65
434,297
12. Usable fuel, main tanks
(0.84 kg/liter) (7.01 lb/US gal)
Lever arm: 2.63 m (103.5 in)
90
198
236.7
20,545
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 6 - 13