Aviation formulas
5 flashcards · Other · by theTisch21
Pressure altitude
alt + 1000 * (std pressure inHg - actual pressure inHg)
Density altitude
PA + 120 * (actual ˚C - standard ˚C)
Maneuvering speed
105 * SQRT(weight/2550)
Pivotal altitude
GS2 / 11.3
DECIDE
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