Tecnam P2010 - Page 472

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 5
Section 5 – Performance-
ICAO STANDARD ATMOSPHERE
Ed. 1, Rev.0
4. ICAO STANDARD ATMOSPHERE
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