The Boeing Company

Homero S Cerna

Tri Minh Phan

Luis Rogelio Gonzalez

Vinh Q Doan

Shu Hsin Robin Hsu

Rickie Lee

Systems, apparatuses and methods may provide for a verification system for an aircraft. The verification system includes a verification function subsystem to automatically verify an operational condition of one or more components of an aircraft based on airflow related signals, hydraulic related signals, and electrical signals and associated impedances and present the operational condition via a display. The airflow related signals may be obtained from a plurality of airflow fittings, the hydraulic related signals may be obtained from a plurality of hydraulic fittings, and the electrical signals and associated impedances may be obtained from a plurality of electrical connectors. At least two of the airflow fittings, at least two of the hydraulic fittings, and at least two of the electrical connectors may be positioned in different aircraft sections before additional aircraft sections are assembled.

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Bothell, WA, United States of America

Homero S Cerna