Boeing 767 Runway Overrun Dynamics Lab FAA KMIA Investigation

Aerodynamic Deceleration, Wet Friction Hydroplaning & Runway Safety Area (RSA) Analysis

Runway & Environment KMIA / MIA
B767-300F Rollout Dynamics CF6-80C2
KMIA RUNWAY OVERVIEW & KINEMATIC ROLLOUT
STATION: 00+00 FT
T+ 0.0s
Operational Safety Determination RUNWAY OVERRUN EXCURSION DETECTED
EXCURSION VELOCITY 31.4 kts
Stopping Distance 13,410 ft Overrun: +394 ft RSA
Peak Deceleration 0.31 G Wheel Brake + Aero Drag
Brake Energy Absorbed 54.2 MWh 195.1 GJ Carbon Discs
Runway Safety Area 39.4% 1,000 ft Buffer Zone
GROUND SPEED VS. RUNWAY DISTANCE (DISTANCE-VELOCITY PROFILE) LDA END AT 13,016 FT
Investigation Audit FAA PART 25
Aircraft Type: B767-300ER BCF
Declared LDA: 13,016 ft
Calculated Stop: 13,410 ft
RSA Margin / Deficit: -394 ft
Overrun Speed: 31.4 kts
Rollout Duration: 38.2 s
Critical Contributing Factor:
Extended touchdown flare (2,650 ft) combined with wet runway surface mu and 8 kt tailwind