Air pressure and air temperature and altitude and airspeed
Intelligence Input Method
Air or electrical
Output Intelligence Type
True air speed and mach number and pressure altitude and temperature
Phase
Single
Frequency In Hertz
400.0
Functional Description
Recieves inputs from the pitot static sub-system, total air temperature probes, barometer setting, and from the aircraft propulsion data management computer. This data is used by the air data computer to compute parameters such as true airspeed, mach number, pressure altitude, and static air temperature which are output on 1553 buses.
