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钻石40飞机飞行手册 DA 40 Airplane Flight Manual(49)

时间:2011-10-28 12:56来源:蓝天飞行翻译 作者:admin
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1. Empty mass (from Mass and Balance Report)  735 1620  1820 158,000 
2. Front seats Lever arm: 2.30 m (90.6 in)  150 331  345 29,989 
3. Rear seats Lever arm: 3.25 m (128.0 in)  150 331  487.5 42,368 
4. Baggage Lever arm: 3.65 m (143.7 in)  0 0  0 0 
5. Total mass and total moment with empty fuel tanks (Total of 1.-4.)  1035 2282  2652.5 230,357 
6. On-board usable fuel (0.84 kg/liter) (7.01 lb/US gal) Lever arm: 2.63 m (103.5 in)  100.8 222  265.10 23,001 
7. Total mass and total moment with full fuel tanks (Total 5. plus 6.)  1135.8 2504  2917.60 253,357 
8. The total moments from rows 5 and 7 (2652.5 and 2917.6 kgm) (230,357 and 253,357 in.lb) must be divided by the related total mass (1035 and 1135.8 kg respectively) (2282 and 2504 lb) and then located in Diagram 6.4.4 'PERMISSIBLE CENTER OF GRAVITY RANGE'. As in our example CG positions (2.562 m and 2.569 m respectively) (100.95 and 101.18 in) and masses fall into the permitted area, this loading condition is allowable. 

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Doc. No. 6.01.05-E  Revision 2  30-Apr-2003  Page 6 - 9 


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CALCULATION OF LOADING CONDITION  DA 40 D (Example)  Your DA 40 D 
Mass [kg] [lb]  Moment [kgm] [in.lb]  Mass [kg] [lb]  Moment [kgm] [in.lb] 
1. Empty mass (from Mass and Balance Report)  735 1620  1820 158,000 
2. Front seats Lever arm: 2.30 m (90.6 in)  150 331  345 29,989 
3. Rear seats Lever arm: 3.25 m (128.0 in)  80 176  260 22,528 
4. Baggage Lever arm: 3.65 m (143.7 in)  0 0  0 0 
5. Total mass and total moment with empty fuel tanks (Tota l of 1.-4.)  965 2127  2425 210,517 
6. On-board usable fuel (0.84 kg/liter) (7.01 lb/US gal) Lever arm: 2.63 m (103.5 in)  100.8 222  265.10 22,977 
7. Total mass and total moment with full fuel tanks (Tota l 5. plus 6.)  1065.8 2349  2690.10 233,494 
8. The total moments from rows 5 and 7 (2425 and 2690.1 kgm) (210,517 and 233,494 in.lb) must be divided by the related total mass (965 and 1065.8 kg respectively) (2127 and 2349 lb) and then located in Diagram 6.4.4 'PERMISSIBLE CENTER OF GRAVITY RANGE'. As in our example CG positions (2.513 m and 2.524 m respectively) (98.97 and 99.40 in) and masses fall into the permitted area, this loading condition is allowable. 


 
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