General Electric Company
Pitot-static air data test system with pilot and co-pilot verification

Abstract:

An Air Data Test System (ADTS) for testing an aircraft pitot-static system including at least one pneumatic pump configured to generate an air pressure, at least two pairs of impact and static ADTS ports, a manifold system in fluid communication with the pneumatic pump and each pair of impact and static ADTS ports, and a signal processor operatively coupled to, and controlling, the at least one pneumatic pump and the manifold system. The signal processor is configured to issue control signals for independently and/or collectively testing each of the pilot and co-pilot pitot-static systems. One pair of ADTS ports is configured to supply air pressure to the pilot pitot-static system and the other pair of ADTS ports is configured to supply air pressure to the co-pilot pitot-static system. A mobile device wirelessly communicates with the signal processor to input the pressure values for testing the pilot and co-pilot pitot-static systems.