DA 40 NG AFM |
Mass & Balance |
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6.4.3 CALCULATION OF LOADING CONDITION
a)Standard Tank Configuration
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DA 40 NG |
Your DA 40 NG |
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(Example) |
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CALCULATION OF |
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Mass |
Moment |
Mass |
Moment |
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LOADING CONDITION |
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[kg] |
[kgm] |
[kg] |
[kgm] |
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[lb] |
[in.lb] |
[lb] |
[in.lb] |
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1. |
Empty mass (from Mass and |
900 |
2,180.8 |
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Balance Report) |
1,984 |
189,253 |
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2. |
Front seats |
150 |
345.0 |
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Lever arm: 2.30 m (90.6 in) |
331 |
29,989 |
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3. |
Rear seats |
0 |
0 |
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Lever arm: 3.25 m (128.0 in) |
0 |
0 |
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4. |
Standard baggage comp. |
20 |
73.0 |
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Lever arm: 3.65 m (143.7 in) |
44 |
6,323 |
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% |
5. |
Baggage tube |
0 |
0 |
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Lever arm: 4.32 m (170.1 in) |
0 |
0 |
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% |
6. Short baggage extension |
0 |
0 |
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% |
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(OÄM 40-331 carried out) |
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% |
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0 |
0 |
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% |
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Lever arm: 3.97 m (156.3 in) |
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% |
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% |
7. Forward extended baggage |
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% |
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compartment (OÄM 40-164 |
0 |
0 |
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% |
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carried out) |
0 |
0 |
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Lever arm: 3.89 m (153.1 in) |
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% |
8. Aft extended baggage |
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% |
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compartment (OÄM 40-164 |
0 |
0 |
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% |
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carried out) |
0 |
0 |
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Lever arm: 4.54 m (178.7 in) |
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Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 6 - 9 |
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Mass & Balance |
DA 40 NG AFM |
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DA 40 NG |
Your DA 40 NG |
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(Example) |
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CALCULATION OF |
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Mass |
Moment |
Mass |
Moment |
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LOADING CONDITION |
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[kg] |
[kgm] |
[kg] |
[kgm] |
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[lb] |
[in.lb] |
[lb] |
[in.lb] |
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% 9. Total mass and total moment |
1,070 |
2,598.8 |
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with empty fuel tanks (Total |
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2,359 |
225,565 |
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% |
of 1.-8.) |
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% 10. On-board usable fuel |
89 |
234.1 |
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(0.84 kg/liter) (7.01 lb/US gal) |
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196 |
20,286 |
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Lever arm: 2.63 m (103.5 in) |
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% 11. Total mass and total moment |
1,159 |
2,832.9 |
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% |
with full fuel tanks (Total 9. |
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2,555 |
245,851 |
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% |
plus 10.) |
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%12. The total moments from rows 9 and 11 2,598.8 and 2,832.9 kgm) (225,565 and 245,851 in.lb) must be divided by the related total mass (1,070 and 1,159 kg respectively) (2,359 and 2,555 lb) and then located in Diagram 6.4.4 - PERMISSIBLE
CENTER OF GRAVITY RANGE.
As in our example CG positions (2.429 m and 2.444 m respectively) (95.62 and 96.22 in) and masses fall into the permitted area, this loading condition is allowable.
Page 6 - 10 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
Mass & Balance |
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b)Long Range Tank Configuration
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DA 40 NG |
Your DA 40 NG |
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(Example) |
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CALCULATION OF |
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Mass |
Moment |
Mass |
Moment |
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LOADING CONDITION |
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[kg] |
[kgm] |
[kg] |
[kgm] |
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[lb] |
[in.lb] |
[lb] |
[in.lb] |
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1. |
Empty mass (from Mass and |
900 |
2,180.8 |
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Balance Report) |
1,984 |
189,253 |
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2. |
Front seats |
150 |
345.0 |
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Lever arm: 2.30 m (90.6 in) |
331 |
29,989 |
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3. |
Rear seats |
0 |
0 |
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Lever arm: 3.25 m (128.0 in) |
0 |
0 |
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4. |
Standard baggage comp. |
20 |
73.0 |
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Lever arm: 3.65 m (143.7 in) |
44 |
6,323 |
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% |
5. |
Baggage tube |
0 |
0 |
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Lever arm: 4.32 m (170.1 in) |
0 |
0 |
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% |
6. Short baggage extension |
0 |
0 |
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% |
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(OÄM 40-331 carried out) |
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% |
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0 |
0 |
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% |
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Lever arm: 3.97 m (156.3 in) |
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% |
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% |
7. Forward extended baggage |
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% |
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compartment (OÄM 40-164 |
0 |
0 |
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% |
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carried out) |
0 |
0 |
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Lever arm: 3.89 m (153.1 in) |
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% |
8. Aft extended baggage |
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% |
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compartment (OÄM 40-164 |
0 |
0 |
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% |
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carried out) |
0 |
0 |
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Lever arm: 4.54 m (178.7 in) |
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Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 6 - 11 |
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Mass & Balance |
DA 40 NG AFM |
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DA 40 NG |
Your DA 40 NG |
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(Example) |
|||
|
CALCULATION OF |
|
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|
Mass |
Moment |
Mass |
Moment |
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LOADING CONDITION |
||||
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[kg] |
[kgm] |
[kg] |
[kgm] |
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||||
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[lb] |
[in.lb] |
[lb] |
[in.lb] |
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% 9. Total mass and total moment |
1,070 |
2,598.8 |
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with empty fuel tanks (Total |
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2,359 |
225,565 |
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% |
of 1.-8.) |
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|
|
|
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% 10. On-board usable fuel |
124 |
326.1 |
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(0.84 kg/liter) (7.01 lb/US gal) |
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|
273 |
28,256 |
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Lever arm: 2.63 m (103.5 in) |
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% 11. Total mass and total moment |
1,194 |
2,924.9 |
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% |
with full fuel tanks (Total 9. |
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2,632 |
253,821 |
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% |
plus 10.) |
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%12. The total moments from rows 9 and 11 (2,598.8 and 2,924.9 kgm) (225,565 and 253,821 in.lb) must be divided by the related total mass (1,070 and 1,194 kg respectively) (2,359 and 2,632 lb) and then located in Diagram 6.4.4 - PERMISSIBLE
CENTER OF GRAVITY RANGE.
As in our example CG positions (2.429 m and 2.450 m respectively) (95.62 and 96.44 in) and masses fall into the permitted area, this loading condition is allowable.
Page 6 - 12 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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