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Printed page 17. PDF page 29.
about 20 percent, where it remained for about 8 seconds. � Autobrakes were deactivated about 12 seconds after touchdown, and pilotcommanded brake pressure increased to 3,000 pounds per square inch (psi). � The first indication of thrust reverser activity wasOpen official document at PDF page 29Runway Overrun and Collision, Southwest Airlines Flight 1248
Printed page 23. PDF page 35.
crew selected MAX autobrakes for the landing and transitioned to maximum manual braking about 12 seconds after touchdown. National Transportation Safety Board 23Open official document at PDF page 35Runway Overrun and Collision, Southwest Airlines Flight 1248
Printed page 51. PDF page 63.
they were not satisfied with the airplane's deceleration, and FDR data indicated that, about 12 seconds after touchdown, they transitioned from autobrakes to maximum manual wheel braking. FDR data indicated that the thrust reversers deployment was initiated 15 seconds aftOpen official document at PDF page 63Runway Overrun and Collision, Southwest Airlines Flight 1248
Printed page 4. PDF page 16.
described by the pilots and indicated that full thrust reverser deployment occurred about 18 seconds after touchdown. However, the airplane ran off the departure end of runway 31C and continued through the runway safety area (RSA),12 a blast fence, aOpen official document at PDF page 16Runway Overrun and Collision, Southwest Airlines Flight 1248