AvPlot
BETA
Acute Angle Exit Design
Fillet Tool ↗ Runway Tool ↗ AC 150/5300-13B Chg 1 ↗
Setup
Exit Entries
Review & Generate
Setup
Name your project and configure exit geometry parameters
Step 1 of 3
AC 150/5300-13B Table 3-6 — based on critical aircraft wheelbase
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.
Project Summary
PROJECT
Name
PARAMETERS
TDG
CMG
Exit Radius R1
Exit Angle
EXITS
Count