Flap | Zero | | 0 | -2.5 | 0 | 2.5 | | Measured at root, down=positive, up=negetive |
| Aileron to Flap | Up | -7.5 | -8 | -7.5 | -6.5 | | |
| | Down | 4 | 4.5 | 4 | 3.5 | 85 deg | |
| Camber | | | | | 7 | | Total camber after adding camber using slider (5-min sink in thermal turn) |
Ailerons | Zero | | 0 | -2.5 | 0 | 2.5 | | Measured at root aileron, down=positive, up=negetive. At zero, ailerons inline with flap |
| Up | | -22 | -25 | -22 | -19 | -9 | |
| Down | | 15 | 18 | 15 | 13 | | |
| Camber | | | | | 7 | | Total camber after adding camber using slider (3.5-min sink in thermal turn) |
| Elevator | Up | 11 | 12 | 11 | 10 | | Up=positive |
| | Down | -15 | -15 | -15 | -15 | -8 | |
| Rudder | | ±32 | ±32 | ±32 | ±34 | | |
| EL->Camber | up (down) | +4 (-4) | +4 (-4) | +5 (-4) | +6 (-3) | | Camber value at root for elevator movement (positive=more camber, trailing edge down) |
| AI->RU | | ±20 | ±15 | ±18 | ±21 | | |
Recommended CG [mm] | 95-100 | | | | | | | CG light battery: 98 mm - CG heavy battery: 96 mm |