⚠ This tool is currently undergoing testing and will be available soon.
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Setup
Name your project and configure exit geometry parameters
AC 150/5300-13B Table 1-4 (TDG Table) — based on critical aircraft wheelbase
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Aircraft wheelbase used in nose-gear steering calculation
Radius of the initial high-speed exit curve — typically 1500 ft
Angle between runway centerline and exit taxiway — typically 30°
Exit Entries
Enter each exit location — runway CL to taxiway CL separation
Review & Generate
Confirm all exits and generate the design report
Ready to Generate
Download the exit design report with geometry for all exits.