A method for providing approach stabilization guidance for an aircraft, the method comprising: at a control module, receiving a published arrival procedure and a published glide path; receiving landing parameters comprising instrument meteorological conditions stabilization altitude, and visual meteorological conditions stabilization altitude; receiving real-time aircraft sensor data; processing the PAP, PGP, landing parameters, and sensor data, to determine a reference approach profile, an actual approach profile, whether the aircraft is following the reference approach profile, and an approach stabilization criterion comprising each of, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC stabilization altitude, (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC), (iii) a wind corrected air mass flight path angle (WC FPA) at the VMC stabilization altitude, and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC); commanding a display system to display a flight management system page having thereon an alphanumeric indication of each of (i) an IMC criterion profile comprising the VS IMC and (ii) a VMC criterion profile comprising the VS VMC; determining, based on the vertical speed at WC FPA IMC and an aircraft deceleration capability, whether (a) the IMC criterion profile stabilizes the actual approach; determining, based on the vertical speed at WC FPA VMC and the aircraft deceleration capability, whether (b) the VMC criterion profile stabilizes the actual approach; and when both the IMC criterion profile stabilizes the actual approach and the VMC criterion profile stabilizes the actual approach: commanding the display system to display "stable"; and allowing user selections of the IMC criterion profile and the VMC criterion profile. receiving a published arrival procedure and a published glide path; receiving landing parameters comprising instrument meteorological conditions stabilization altitude, and visual meteorological conditions stabilization altitude; receiving real-time aircraft sensor data; processing the PAP, PGP, landing parameters, and sensor data, to determine a reference approach profile, an actual approach profile, whether the aircraft is following the reference approach profile, and an approach stabilization criterion comprising each of, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC stabilization altitude, (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC), (iii) a wind corrected air mass flight path angle (WC FPA) at the VMC stabilization altitude, and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC); commanding a display system to display a flight management system page having thereon an alphanumeric indication of each of (i) an IMC criterion profile comprising the VS IMC and (ii) a VMC criterion profile comprising the VS VMC; determining, based on the vertical speed at WC FPA IMC and an aircraft deceleration capability, whether (a) the IMC criterion profile stabilizes the actual approach; determining, based on the vertical speed at WC FPA VMC and the aircraft deceleration capability, whether (b) the VMC criterion profile stabilizes the actual approach; and when both the IMC criterion profile stabilizes the actual approach and the VMC criterion profile stabilizes the actual approach: commanding the display system to display "stable"; and allowing user selections of the IMC criterion profile and the VMC criterion profile. a reference approach profile, an actual approach profile, whether the aircraft is following the reference approach profile, and an approach stabilization criterion comprising each of, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC stabilization altitude, (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC), (iii) a wind corrected air mass flight path angle (WC FPA) at the VMC stabilization altitude, and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC); commanding a display system to display a flight management system page having thereon an alphanumeric indication of each of (i) an IMC criterion profile comprising the VS IMC and (ii) a VMC criterion profile comprising the VS VMC; determining, based on the vertical speed at WC FPA IMC and an aircraft deceleration capability, whether (a) the IMC criterion profile stabilizes the actual approach; determining, based on the vertical speed at WC FPA VMC and the aircraft deceleration capability, whether (b) the VMC criterion profile stabilizes the actual approach; and when both the IMC criterion profile stabilizes the actual approach and the VMC criterion profile stabilizes the actual approach: commanding the display system to display "stable"; and allowing user selections of the IMC criterion profile and the VMC criterion profile. commanding the display system to display "stable"; and allowing user selections of the IMC criterion profile and the VMC criterion profile.