| Flaps | Zero | 0 | 2 | 3,5 | -0,5 | 1,5 | 60 | Measured at root, down =positive, up=negative |
| Up | 5 | 3 | -1 | 5 | | 10 | Flap to butterfly mix reduces flaps when more than half sticks is used |
| Down | 5 | 4 | 5 | 3 | | 35 | Flap to butterfly mix reduces flaps when more than half sticks is used |
| Super thermal
| -- | -- | 7 | -- | | -- | Total camber after adding camber using slider |
| Ailerons | Zero | 0 | 2 | 4 | -0,5 | 1,5 | 25 | Measured at root, down=positive, up=negative |
| Up | 15 | 12 | 9 | 16 | | -20 | Aileron to butterfly mix reduces flaps when more than half sticks is used |
| Down | 12 | 10 | 7 | 14 | | 5 | Aileron to butterfly mix reduces flaps when more than half sticks is used |
| Super thermal | -- | -- | 6 | -- | | -- | Total camber after adding camber using slider |
| Elevator | Zero | -0,25 | 0 | 0,25 | -0,25 | 1
| -5 | Up=positive |
| Up | 9 | 8 | 7,5 | 8,5 | | -- | |
| Down | 15 | 15 | 15 | 15 | | | |
Rudder
| Left / right | 16 | 16 | 14 | 0 | | -- | |
Elevator - Camber
| Up / down | +5 (-3) | +5 (-1,5) | +6 (0) | +4 (-4) | | -- | Delta flap for elevator movement (positive=more camber) |
| Aileron - Rudder | | 2,5 | 3 | 2,5 | 2,5 | | Max | |
| Recommended CG [mm] | 70 - 69 mm | | | | | | | From leading edge at root |
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