AirplanePDQ
Weight and Balance Report
| Design Name: | Vision_4 |
| Designer: | Jim Shafer |
| Design Date: | 031002 |
Weight Breakdown
| Parameter |
Weight |
Station |
| SI Units |
User Units |
SI Units |
User Units |
| Structures Group |
|
| Main Wing |
101. kg |
222.6 lbm |
2.171 m |
85.47 in |
| Horizontal Stabilizer |
18.87 kg |
41.61 lbm |
5.987 m |
235.7 in |
| Vertical Stabilizer |
5.193 kg |
11.45 lbm |
5.956 m |
234.5 in |
| Fuselage |
98.82 kg |
217.9 lbm |
2.436 m |
95.92 in |
| Landing Gear |
50.36 kg |
111. lbm |
1.761 m |
69.32 in |
| Propulsion Group |
|
| Engine #1 |
172.4 kg |
380. lbm |
0.5592 m |
22.01 in |
| Fuel System |
20.2 kg |
44.54 lbm |
2.009 m |
79.1 in |
| Equipment Group |
|
| Avionics |
35.59 kg |
78.45 lbm |
1.538 m |
60.54 in |
| Electrical |
48.9 kg |
107.8 lbm |
0.9027 m |
35.54 in |
| Flight Controls |
30.36 kg |
66.93 lbm |
2.436 m |
95.92 in |
| Furnishings |
41.26 kg |
90.96 lbm |
1.954 m |
76.92 in |
| TOTAL WEIGHT EMPTY |
622.9 kg |
1,373.2 lbm |
1.739 m |
68.45 in |
| Useful Load Group |
|
| Crew and Passengers |
326.6 kg |
720. lbm |
2.445 m |
96.26 in |
| Fuel |
212.8 kg |
469.2 lbm |
2.009 m |
79.1 in |
| Cargo |
22.68 kg |
50. lbm |
3.225 m |
127. in |
| AS-DRAWN GROSS WEIGHT |
1,185. kg |
2,612.4 lbm |
2.01 m |
79.15 in |
CG Limits
| Parameter |
SI Units |
User Units |
| Forward CG Limit |
1.765 m |
69.49 in |
| Aft CG Limit |
2.128 m |
83.79 in |
| Neutral Point |
2.231 m |
87.84 in |
| Forward CG Limit (%MAC) |
8.369 |
| Aft CG Limit (%MAC) |
36.68 |
| Neutral Point (%MAC) |
44.68 |
Loading Extremes
| Parameter |
CG Location |
Static Margin |
| SI Units |
User Units |
% MAC |
| Most Forward CG Loading |
1.777 m |
69.97 in |
35.37 |
|
| Most Aft CG Loading |
2.011 m |
79.16 in |
17.18 |
|