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 () required for this runway. Apply the standard FAA corrections sequentially.
Solution: Runway Length Correction
0 of 4 Steps Completed1
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 () = 6,000 ft
- Elevation = 3,000 ft
- Correction rate = 7% per 1,000 ft
Step-by-Step Solution
0 of 2 Steps Completed1