DA20-C1 Flight Manual
Supplement 4
Doc # DA202-C1 April 16, 2009 Page S4 - 10
SENSENICH PROPELLER W69EK7-63, W69EK7-63G and W69EK-63
Best Rate-of-Climb Speed with Wing Flaps T/O 68 KIAS
Example: Pressure Altitude: 2000 ft
OAT: 65º F
Weight : 1764 lbs
Result: Climb performance: 744 ft/min
Figure 5.7. Climb Performance / Take off
Revision 24 DOT Approved