Flight Load Inputs
Calculated Results
Total Weight: Max 472.5 kg
- kg
Remaining Weight Margin:
- kg
Center of Gravity (XCG): 1.50m - 1.70m
- m
Mathematical Formulas
Reference Formula
XCG =
(WAE·XAE) + (Wcrew·Xcrew) + (Wfuel·Xfuel) + (Wbag·Xbag)
WAE + Wcrew + Wfuel + Wbag
Live Current Values
XCG =
(295×1.5) + (0×1.6) + (0×2.0) + (2×2.3)
295 + 0 + 0 + 2
Aircraft Constants & Specifications
| Variable | Meaning | Default value |
|---|---|---|
| WAE | Actual empty weight of the airplane | 472.5 Kg |
| XAE | CG position of the empty airplane | 1.50 m |
| Wcrew | Total weight of pilots | — |
| Xcrew | Position of pilots' CG | 1.6 m |
| Wfuel | Total weight of fuel in the tanks | — |
| Xfuel | Position of fuel tank CG | 2.0 m |
| Wbag | Weight of the baggage in the baggage container | — |
| Xbag | Position of the baggage CG | 2.3 m |
