This SAE Aerospace Standard (AS) covers air data computer equipment (hereinafter designated the computer) which when connected to sources of aircraft electrical power, static pressure, total pressure, outside air temperature, and others specified by the manufacturer (singly or in combination) provides some or all of the following computed air data output signals (in analog and/or digital form) which may supply primary and/or standby flight instruments:
Pressure Altitude
Pressure Altitude, Baro-Corrected
Vertical Speed
Calibrated Airspeed
Mach Number
Maximum Allowable Airspeed
Over-speed Warning
Total Air Temperature
