Diamond DA20-C1 - 2.16. DEMONSTRATED CROSSWIND COMPONENT; 2.17. TEMPERATURE LIMITS

DA20-C1 Flight Manual Limitations
Doc # DA202-C1 April 06, 2010 Page 2 - 20
57. On the instrument panel. If equipped with altitude compensating fuel pump.
2.16. DEMONSTRATED CROSSWIND COMPONENT
The maximum demonstrated crosswind component is 20 kts. (37 km/h).
2.17. TEMPERATURE LIMITS
CAUTION
FOR AIRCRAFT WITH OTHER THAN WHITE UNDERSIDES.
PARKING THE AIRCRAFT OVER A LIGHT COLOURED OR
REFLECTIVE SURFACE IN CONDITIONS OF BRIGHT
SUNLIGHT, PARTICULARLY AT HIGH OAT, IS NOT
RECOMMENDED.
Temperature limit of the structure for the operation of the airplane:
Maximum T/O Temperature : 131°F (55°C)
Structural Temperature
Revision 25 DOT Approved