Flight & Runway Parameters
148 kts
Vref 138 kts+10 kt gust factor175 kts
1,850 ft
Nominal TDZ (1,000–1,500 ft)Late Float (3,500 ft)
295,000 lbs
MLW ~300,000 lbs (Boeing 767-300F)
0.22 (μ)
0.10 Standing Water0.30 Wet Grooved0.50 Dry
-8 kts (Tailwind)
-18 kt Tailwind0 Calm+25 kt Headwind
Autobrake Mode
Mode 3
1 (Mild)
2 (Mod)
3 (Med-Heavy)
4 (Heavy)
MAX AUTO
MANUAL FULL
KMIA RUNWAY DECELERATION SCHEMATIC (SCALE 1:20)
[SIM ACTIVE]
Approach/Touchdown
Spoilers / Brakes
Thrust Reversers
Overrun Excursion
Safe Stop Area
Stopping Distance
-- ft
Threshold to full stop
Runway Margin / Excursion
-- ft
Distance relative to pavement end
Threshold Excursion Velocity
0 kts
Ground speed crossing runway end
Kinetic Energy Dissipation
-- MJ
Total rollout work required
RSA Buffer Incursion
0 ft
Soil penetration depth (1,000 ft buffer)
Speed Profile & Energy Boundary (Knots vs. Distance in Feet)
KMIA RUNWAY PROFILE
Deceleration Forces (Aerodynamic, Wheel Brak