Quick Reference Values
Aircraft Classification Number Pavement Classification NumberACN/PCN system as defined by ICAO Annex 14 is adopted for load characterization.
Design Life YearsTypically 20 years for flexible pavements, but can be extended based on economic analysis.
Subgrade CBR MinimumMinimum CBR of 5 percent for design purposes, with adjustments for seasonal variations.
Subgrade Modulus K ValueValues ranging from 30 MPa/m to 100 MPa/m depending on soil type and moisture content.
Granular Sub Base Minimum ThicknessMinimum thickness of 150 mm, subject to traffic and subgrade conditions.
Granular Base Minimum ThicknessMinimum thickness of 150 mm, subject to traffic and subgrade conditions.
Asphalt Concrete Surface Minimum ThicknessMinimum thickness of 50 mm for primary runways, potentially higher for critical areas.
Asphalt Concrete Mix TypeDense-graded asphalt concrete (e.g., AC 10, AC 20) is commonly specified.
Bitumen GradePenetration grades (e.g., 40/60, 60/70) or Viscosity grades (e.g., VG-30, VG-40) are specified based on climate.
California Bearing Ratio CBRA primary parameter for subgrade strength, used in design charts and calculations.
Resilient Modulus MrIncreasingly used as an alternative or complementary parameter to CBR, especially for newer materials.
Traffic Sub DivisionsRunways are categorized into different traffic categories based on aircraft type and frequency (e.g., Code 3, Code 4, Code 5).
Repetition Factor NCumulative number of repetitions of the critical aircraft load over the design life.
Load Magnitude Factor LAccounts for the magnitude of the aircraft load relative to a standard load.
Contact PressureTypically between 1.0 MPa and 1.5 MPa for modern aircraft tires.
Annual Rate of Increase in TrafficConsidered for future traffic projections.
Temperature Correction Factor TcApplied to asphalt properties to account for variations in ambient temperature.
Drainage Coefficient CdAccounts for the impact of water on pavement performance, with values typically ranging from 0.8 to 1.0.
Key Formulas
ACN = (Aircraft Gross Mass x Load Factor) / Standard Load
ESWL = f(Tire Pressure, Load, Layer Properties)
SN = a1*D1 + a2*D2 + a3*D3
N_eq = (N_traffic / N_design) ^ (1/beta)