AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGRATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 5-5
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
Ed. 1, Rev. 0
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