DA20-C1 Flight Manual
Supplement 4
Doc # DA202-C1 April 16, 2009 Page S4 - 11
SENSENICH PROPELLER W69EK7-63, W69EK7-63G and W69EK-63
Diagram for true airspeed (TAS) calculation at selected power level.
Example: Pressure altitude: 6000 ft.
Temperature: 70º F
Power setting: 65%
Result: True airspeed (TAS): 121kts
Figure 5.8. Cruising Speed (True Airspeed)
Revision 24 DOT Approved