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.

Abstract: A system for verifying an aircraft instrumentation value comprising: an Air Data Test Module (ADTM) configured to pneumatically simulate at least one instrumentation value based upon a pressure set-point. The pneumatically simulated instrumentation value corresponds to the pressure set point and is reported by an aircraft transponder. A receiver module receives the pneumatically simulated instrumentation value transmitted by the aircraft transponder. A signal processor, is operative to (i) control the ADTM, (ii) command a prescribed instrumentation value to be simulated by the ADTM, (iii) compare the prescribed instrumentation value to the pneumatically simulated instrumentation value, and (iv) issue a pass signal when the values match, and a fail signal when the values differ by a threshold value.

Abstract: A system for verifying an aircraft instrumentation value comprising: an Air Data Test Module (ADTM) configured to pneumatically simulate at least one instrumentation value based upon a pressure set-point. The pneumatically simulated instrumentation value corresponds to the pressure set point and is reported by an aircraft transponder. A receiver module receives the pneumatically simulated instrumentation value transmitted by the aircraft transponder. A signal processor, is operative to (i) control the ADTM, (ii) command a prescribed instrumentation value to be simulated by the ADTM, (iii) compare the prescribed instrumentation value to the pneumatically simulated instrumentation value, and (iv) issue a pass signal when the values match, and a fail signal when the values differ by a threshold value.

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.