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.
