The Airline Pilots Forum and Resource
THE AIRLINE PILOTS FORUM & RESOURCE
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Engine Out Climb and Turn
QNH (hPa):
OAT (°C):
Wind Component (knots):
HW
TW
Bank Angle (degrees):
Runway Elevation (feet):
Acceleration Altitude (feet):
V2 (KIAS):
Climb Gradient (%):
Calculate
This app is designed for engine failure performance evaluation during takeoff, using TAS calculated at a mean elevation between the runway and acceleration altitude. Accuracy may vary if used for other purposes.
Airline Pilots Forum and Resource