Flight Manual STEMME S6
Doc.-No.:P400-006.000 E Page: 5-10 Revision: ---
Date of Issue: 07. October 2008 Agency approved Date of Rev.: --.--.----
Caution: In the glider-configuration stall warning for the pilot is ONLY
through aerodynamic buffeting. The onset of buffeting begins
about 3 to 4 kts / 5 to 8 km/h above the stall.
Note: If the CG-location is far aft, then slightly lower stall speeds
might be reached. The aircraft might drop a wing
downwards, even if the flight controls are not against the aft
stop.
5.3.5 Wind-Components
• The maximum demonstrated crosswind-component
for taxi, take-off and landing is: 16 kts / 30 km/h