Example: Runway Length Correction

Example

Problem Statement: A new airport is being designed at an elevation of 3,000 feet above MSL. The critical design aircraft requires a basic runway length of 6,000 feet under standard sea level conditions. The Airport Reference Temperature (ART) is 25.0°C. The proposed runway has an effective gradient of 0.5%.
Calculate the final actual design length (LactualL_{actual}) required for this runway. Apply the standard FAA corrections sequentially.

Solution: Runway Length Correction

0 of 4 Steps Completed
1

Example: Basic Runway Length Calculation

Runway length is dictated by aircraft performance, temperature, and elevation.

Example

Problem Statement: An aircraft requires a basic runway length of 6,000 ft at standard sea-level conditions. The proposed airport is located at an elevation of 3,000 ft. Applying the standard FAA elevation correction (increase length by 7% per 1,000 ft of elevation), calculate the corrected runway length.
Given:
  • Basic Length (LbL_b) = 6,000 ft
  • Elevation = 3,000 ft
  • Correction rate = 7% per 1,000 ft

Step-by-Step Solution

0 of 2 Steps Completed
1