DA 40 NG AFM |
Mass & Balance |
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6.4.4 PERMISSIBLE CENTER OF GRAVITY RANGE
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The CG’s shown in the diagram are from the examples in Tables 6.4.3 -
CALCULATION OF LOADING CONDITION a) and b), rows 6 and 8.
The flight CG position must be within the following limits:
Most forward CG:
2.40 m (94.5 in) aft of DP from 940 kg to 1080 kg (2072 lb to 2381 lb)
2.46 m (96.9 in) aft of DP at 1280 kg (2822 lb) linear variation between these values
Most rearward CG:
2.53 m (99.6 in) aft of DP from 940 kg (2072 lb) to 1280 kg (2822 lb)
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 6 - 13 |
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Mass & Balance |
DA 40 NG AFM |
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6.4.5 PERMISSIBLE MOMENT RANGE |
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FlightMass(lb) |
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2900 |
2800 |
2700 |
2600 |
2500 |
2400 |
2300 |
2200 |
2100 |
2000 |
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Flight Mass Moment (in.lb) |
200,000 220,000 240,000 260,000 280,000 |
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Max. Zero Fuel Mass |
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Example Long Range Tank |
Example Standard Tank |
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2200 2400 2600 2800 3000 3200 |
Flight Mass Moment (kgm) |
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1300 |
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1200 |
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1100 |
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1000 |
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900 |
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FlightMass(kg) |
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Page 6 - 14 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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