| Takeoff | The wing goes to normal flight position steadily. Slight brake application demanded in the vicinity of normal takeoff wing position. No hard points found. |
| Landing | Good speed gain, good approach |
| Speed range | Brakes only: 17 km/h. Brakes and accessory: 24 km/h. |
| Pitch stability test | The wingtips are stalling first. Pitch energical but moderate in amplitude |
| Brakes parachuting test | No parachuting phase found. Return to normal speed is very steady. Spontaneous return to normal flight with slight, well-damped pitch |
| B-stall, slow release | Spontaneous return to normal flight with slight, well-damped pitch |
| B-stall, fast release | Spontaneous return to normal flight. Pitch energical but small in amplitude |
| Ability of turn, 360° | Very good roll behaviour. Small brake application demanded. Very good change of turn direction. No weight shift demanded |
| Maneuverability test | Partial stall of inner wing part. Returns to normal flight with average pitch |
| Wing over | Very good roll behaviour. Wingtips are very solid against tucks |
| Asymmetrical tuck | Very difficult maneuver because of particularities of wing profile. After a 60% inflation the wing performs a quick pitch and turn. Returns to normal flight spontaneously after a turn below 90° |
| Asymmetrical tuck (maintained) | Immediate beginning of turn. Spontaneous return to normal flight |
| Negative spin | Spontaneous return to normal flight after 3/4 turn. Pitch is average, very damped and not causing an inflation |
| Asymmetrical stall | Well-damped average pitch. Spontaneous return to normal flight |
| Symmetrical tuck | The middle of the wing could not be iinflated because of the particluratites of wing profile. The A and B-risers load is very high, including wing tips. Inflation spontaneous and very quick |
| Spiral dive | Spontaneous return to normal flight after one turn. No brake application demanded |
