1
Q
Moment
A
M=Arm x Force
2
Q
Pressure altitude
A
PA = [(29.92 - Current Pressure) x 1000 ] + Airport Elevation
3
Q
Density altitude
A
DA = [(Local Temperature) - (Standard Temp)]x120 + Pressure Altitude
4
Q
Standard day
A
At sea level, Altimeter:29.92 in/Hg at 15 °C (59 °F)
Faa Private Piolt Test
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