KMIA / MIA

Aircraft Landing Rollout & Runway Overrun Dynamics Simulator

Grounded in FAA Safety Reports • KMIA Runway Safety Area (RESA) Physics
KMIA Runway Top-Down Rollout Simulation
0.00 s 0 ft
Total Stopping Distance
0 ft
from physical threshold
Runway Margin (Safety Area)
+0 ft
Calculating...
Kinetic Energy Dissipated
0 MJ
Brakes, Aero Drag & Reversers
Peak Deceleration
0.00 G
Rollout duration: 0.0s
Braking Telemetry Curve: Velocity (kts) & Deceleration vs Distance Past Threshold
─ Groundspeed (kts)  •  ─ Decel (ft/s²)  •  | Runway End
INVESTIGATIVE CONTEXT Miami International Airport (KMIA) Cargo Flight Overrun Incident

Incident Summary: According to the Federal Aviation Administration (FAA) and ABC News reports, a cargo aircraft arriving from Puerto Rico overran the runway at Miami International Airport on a Sunday afternoon. Convective tropical storm weather in South Florida frequently produces sudden heavy rain showers, wet pavement with standing water, reduced tire-pavement friction coefficients (μ ≤ 0.20), and sudden tailwind shifts during convective downbursts.

Educational Physics Notice: This model calculates rigid-body kinetic energy dissipation ($E_k = \frac{1}{2}m v^2$), aerodynamic lift dump via spoilers, wheel braking friction force ($F_{\text{friction}} = \mu_{\text{eff}} [W - L_{\text{aero}}]$), and reverse thrust curves. It is designed to teach aeronautical stop-distance factors and is not an official NTSB accident reconstruction.

Side-by-Side Run Comparison Capture Run A and Run B to test risk trade-offs
Slot Runway Cond (μ) Vtd / Wind TD Point Stop Dist Margin Outcome
Run A RWY 8L (8,600') Wet (μ=0.22) 148 kt / +8 kt TW 1,850' -- -- Unset
Run B RWY 8L (8,600') Dry (μ=0.55) 135 kt / -5 kt HW 1,200' -- -- Unset