Tecnam P2010 - Page 294

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V5-5
4. ICAO STANDARD ATMOSPHERE
FIG. 5-2. ICAO CHART
Examples:
Scope Given Find
Density Altitude:
A: Pressure altitude = 1600ft
B: Temperature = 20°C
→
C: Density Altitude = 2550ft
ISA Temperature: D: Pressure altitude = 1600ft
→
E: ISA Air Temperature = 12°C
Section 5 - Performances
ICAO STANDARD ATMOSPHERE
2
nd
Edition, Rev. 0