The airspeed indicator can optionally be configured to display V_ne adjusted for true airspeed and allow the pilot of the aircraft to maintain situational awareness of the TAS V_ne. This is useful in aircraft where true airspeed (instead of indicated airspeed) must be kept below V_ne. When accounting for altitude and temperature, the TAS of the aircraft may be greater than the indicated airspeed. If configured, the AXIS™ flight displays can calculate and display this reduction in V_ne. As TAS increases with the altitude and temperature calculations, a solid red band is displayed between the TAS adjusted V_ne and the actual indicated value for V_ne.