No airflow in this figure — just the aircraft and the two pins that decide whether it flies. Flip between A, the aircraft as designed, and D, the buildable canard-less low-wing arrangement: the canard leaves (its 10 kg carved with it), the wing drops 412 mm with its nacelles riding it, the crew rise onto the pack — and the grey centre-of-gravity pin and the blue neutral-point pin trade places. That trade is the whole story: in A the neutral point sits 11 mm ahead of the CG (−1.2% — the margin is not there); in D it stands 122 mm behind it (+13.2% — a stable aircraft). Pin stations are the measured values, drawn to true scale.
| Neutral point | – |
| Solo-pilot CG | – |
| NP − CG | – |
| Flare reserve, flaps full, α12 | – |
| Prop disk above runway | – |
| Rotation to prop strike | – |