An aircraft-based runway overrun awareness alerting system, comprising: one or more processors installable aboard an aircraft and configured for: determining a plurality of sequential position states corresponding to the aircraft, each position state associated with an inflight position of the aircraft and a direction of the aircraft; determining one or more runway attributes corresponding to a runway proximate to the aircraft; determining a plurality of sequential energy states of the aircraft, wherein each energy state includes an angle of attack and an airspeed; predicting, based on the plurality of position states, the plurality of energy states, and the one or more runway attributes, a plurality of sequential landing points on the proximate runway, and whether, given the plurality of energy states and the plurality of position states, the predicted landing point is trending forward or backward relative the runway; predicting, based on at least the plurality of landing points and the plurality of energy states, at least one trend corresponding to a runway overrun probability; and revising at least one of the plurality of landing points and the predicted trend based on one or more of a change in the plurality of position states and a change in the plurality of energy states, and at least one display device in communication with the one or more processors, the display device configured to: display, within a display surface, one or more of a primary flight display "PFD" component and a navigational instrument corresponding to the aircraft; and display at least one dynamic graphic representation corresponding to the predicted trend, the dynamic graphic representation not integrated with the one or more of the PFD component and the navigational instrument and wherein the dynamic graphic representation is configured to change in shape to reflect trending away towards a safe landing or toward a runway overrun. one or more processors installable aboard an aircraft and configured for: determining a plurality of sequential position states corresponding to the aircraft, each position state associated with an inflight position of the aircraft and a direction of the aircraft; determining one or more runway attributes corresponding to a runway proximate to the aircraft; determining a plurality of sequential energy states of the aircraft, wherein each energy state includes an angle of attack and an airspeed; predicting, based on the plurality of position states, the plurality of energy states, and the one or more runway attributes, a plurality of sequential landing points on the proximate runway, and whether, given the plurality of energy states and the plurality of position states, the predicted landing point is trending forward or backward relative the runway; predicting, based on at least the plurality of landing points and the plurality of energy states, at least one trend corresponding to a runway overrun probability; and revising at least one of the plurality of landing points and the predicted trend based on one or more of a change in the plurality of position states and a change in the plurality of energy states, and determining a plurality of sequential position states corresponding to the aircraft, each position state associated with an inflight position of the aircraft and a direction of the aircraft; determining one or more runway attributes corresponding to a runway proximate to the aircraft; determining a plurality of sequential energy states of the aircraft, wherein each energy state includes an angle of attack and an airspeed; predicting, based on the plurality of position states, the plurality of energy states, and the one or more runway attributes, a plurality of sequential landing points on the proximate runway, and whether, given the plurality of energy states and the plurality of position states, the predicted landing point is trending forward or backward relative the runway; predicting, based on at least the plurality of landing points and the plurality of energy states, at least one trend corresponding to a runway overrun probability; and revising at least one of the plurality of landing points and the predicted trend based on one or more of a change in the plurality of position states and a change in the plurality of energy states, and at least one display device in communication with the one or more processors, the display device configured to: display, within a display surface, one or more of a primary flight display "PFD" component and a navigational instrument corresponding to the aircraft; and display at least one dynamic graphic representation corresponding to the predicted trend, the dynamic graphic representation not integrated with the one or more of the PFD component and the navigational instrument and wherein the dynamic graphic representation is configured to change in shape to reflect trending away towards a safe landing or toward a runway overrun. display, within a display surface, one or more of a primary flight display "PFD" component and a navigational instrument corresponding to the aircraft; and display at least one dynamic graphic representation corresponding to the predicted trend, the dynamic graphic representation not integrated with the one or more of the PFD component and the navigational instrument and wherein the dynamic graphic representation is configured to change in shape to reflect trending away towards a safe landing or toward a runway overrun.