Tecnam P2006T - Page 150

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Section 5 - Performances
ICAO STANDARD ATMOSPHERE
4
th
Edition, Rev. 0
4. ICAO STANDARD ATMOSPHERE
Figure 2 – ICAO chart
5. EXAMPLES:
Given
Find
a. Temperature = 20°C
b. Pressure altitude = 1600’
c. Corresponding Density Altitude = 2250’
Given
Find
A. Pressure altitude = 1600’
ISA condition
B. ISA Air Temperature = 12°C
c.δA=2250 ft
A.δA=1600 ft
B. °C