Sections
Any field left blank will be filled with a zero, except the Runway Length and the Altimeter Setting field.
The computed values of 2nd segment gradients and final segment gradients include headwind corrections.
When computing a takeoff with a required SID gradient or an obstacle the final segment gradient is computed at the appropriate altitude and temperature, not at the departure field elevation and temperature.
The maximum continuous thrust is always computed at the Gross Leveloff Height and temperature (400 ft minimum).
For Obstacles: Enter the obstacle's True height and distance from DER in feet.
For SID gradients: Enter the required SID gradient in feet/Nautcal Miles, and the required SID altitude in feet.
The program will perform runway optimization before displaying the final results in order to present the optimum takeoff weight.