| | | Launch | Speed | Cruize | Thermal | Land | Remarks |
| Flap | Zero | | 2 | 0 | 2 | 4.5 | 0 | Measured at root, down=positive, up=negetive |
| Aileron to flap | Up | -3.5 | -9 | -6 | 0 | | |
| | Down | 6 | 6 | 7 | 6 | | |
| Camber | | | | | 8 | 85deg | Total camber after adding camber using slider (4-min sink in thermal turn) |
| Ailerons | Zero | | 2 | 0 | 2 | 4 | | Measured at root aileron, down=positive, up=negetive |
| Up | | -15 | -24 | -20 | -14 | 0 | |
| Down | | 13 | 17 | 17 | 14 | | |
| Camber | | | | | 7 | -6 | Total camber after adding camber using slider (3.5-min sink in thermal turn) |
| Elevator | Zero | 0 | -0.25 | 0 | 0.25 | 0 | Up=positive |
| | Up | 14 | 14 | 12 | 10.5 | | |
| | Down | -12 | -14 | -14 | -14 | -8 | |
| Rudder | | ± 33 | ± 33 | ± 33 | ± 30 | | |
| Elevator to Flap | up (down) | +5 (-5) | +5 (-6) | +5 (-5) | +5 (-4) | | Camber value at root for elevator movement (positive=more camber, trailing edge down) |
| | | +4.5 (-4.5) | +4 (-5.5) | +4.5 (-4.5) | +4.5 (-3.5) | | Camber value at aileron root for elevator movement (positive=more camber, trailing edge down) |
| Aileron to Rudder | | ±12 | ±7 | ±20 | ±18 | | |
| Recommended CG [mm] | 108-112 | | | | | | | Usable range is 100-120 mm |
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