7. At speed 50 km/h (30 kt) smoothly p control stick back to lift front wheel. The aircraft will lift-o at 70 km/h (40
kt)
8. Level o aircraft at 3 ft above the ground, until reaching 90 km/h (48 kt)
9. Climb at 110 km/h (60 kt) ; engine speed max. 5800 RPM (for max. 5 min)
10. Flaps retract at altitude 50 m (150 ft) AGL, than climb at 120 km/h (65kt) airspeed (at 5500 RPM)
11. Engine instruments – check values
12. EMS - display - check for any error messages
13. Trim – adjust as required to reduce control stick forces
4.7.3. Soft eld takeo
Apply Normal takeo procedures (according to Art. 4.7.1), but:
• Perform a Holding point procedure Checks (according to Art. 4.6) before start to taxy
• Do NOT stop at holding point, line up straight on runway and perform takeo
4.8. Climbing
Rotax 912 ULS
Climbing
3,9 m/s
768 fpm
At speed 120 km/h (65kt)
4.9. Cruise
1. Set aircraft to horizontal ight
2. Trim - as required to reduce control stick forces
3. Fuel pump - switch “OFF”
4. Fuel pressure - check value
5. Throttle and propeller angle - set as required
• 4300 rpm at 26.3 inHG Manifold pressure
• 4800 rpm at 26.5 inHG Manifold pressure
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