Diamond DA 42 - Calculation of Loading Condition

DA 42 AFM Mass and Balance
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017 Page 6 - 11
CALCULATION OF
LOADING CONDITION
DA 42 (Example) Your DA 42
Mass
[kg]
[lb]
Moment
[kgm]
[in.lb]
Mass
[kg]
[lb]
Moment
[kgm]
[in.lb]
1. Empty mass (from Mass and
Balance Report)
1250
2756
2937.5
254,965
2. Front seats
Lever arm: 2.30 m (90.6 in)
160
353
368.0
31,982
3. Rear seats
Lever arm: 3.25 m (128.0 in)
70
154
227.5
19,712
4. Nose baggage compt.
Lever arm: 0.60 m (23.6 in)
5
11
3.0
260
5. Cabin baggage compt.
Lever arm: 3.89 m (153.1 in)
10
22
38.9
3,368
6. Baggage extension
Lever arm: 4.54 m (178.7 in)
5
11
22.7
1,966
7. De-Icing fluid (if installed; see
NOTE on previous page)
(1.1 kg/liter) (9.2 lb/US gal)
Lever arm: 1.00 m (39.4 in)
27.5
61
27.5
2,403
8. Total mass & total moment
with empty fuel tanks
(Total of 1. through 7.)
Note: Maximum zero fuel masses:
-1650 kg (3638 lb)
-1674 kg (3690 lb) if OÄM 42-188 is
carried out
-1730 kg (3814 lb) if OÄM 42-188 and
OÄM 42-195 are carried out
1527.5
3368
3625.1
314,656
9. Usable fuel, main tanks
(0.84 kg/liter) (7.01 lb/US gal)
Lever arm: 2.63 m (103.5 in)
159
351
418.2
36,329