Specifications

SECTION VII
FLIGHT PLANNING AND PERFORMANCE
MODEL 560
Figure 7-4. Fuel Loading Weight and Moment Table
FORM NUMBER 2062, 23 March 2000
FUEL LOADING WEIGHT AND MOMENT TABLE
WEIGHT
(POUNDS)
MOMENT/100
ARM VARIES
(INCH-POUNDS)
3100 9300.31
3200 9604.80
3300 9909.90
3400 10214.96
3500 10520.65
3600 10827.36
3700 11134.04
3800 11441.42
3900 11749.53
4000 12058.00
4100 12366.42
4200 12675.18
4300 12984.28
4400 13293.28
4500 13602.60
4600 13911.78
4700 14221.26
4800 14530.56
4900 14840.14
5000 15149.50
5100 15459.12
5200 15769.00
5300 16078.61
5400 16388.46
5440 16512.58
WING TANK FUEL (CONTINUED)
WING TANK FUEL
WEIGHT
(POUNDS)
MOMENT/100
ARM VARIES
(INCH-POUNDS)
100 292.05
200 582.24
300 872.52
400 1165.28
500 1459.60
600 1755.42
700 2052.05
800 2349.84
900 2648.07
1000 2947.10
1100 3246.76
1200 3546.60
1300 3847.22
1400 4147.92
1500 4449.15
1600 4750.88
1700 5052.57
1800 5354.46
1900 5657.06
2000 5959.60
2100 6262.20
2200 6565.24
2300 6868.49
2400 7171.68
2500 7475.25
2600 7779.20
2700 8083.26
2800 8387.12
2900 8691.30
3000 8995.80
I 7-8 Configuration AA 56OMB-01