AIRCRAFT SYSTEM WIRING DIAGRAM Sample Clauses

AIRCRAFT SYSTEM WIRING DIAGRAM. HI shall prepare a System wiring diagram, showing the entire System wiring definition, equipment pin assignments, grounds, etc., in a format following the airline Customer layout and symbology, and executed per ATA 100. Diagrams shall be readable from left to right in reference to power, control, actuation, and indication. The diagrams shall be based on the following Aircraft condition: Aircraft on the ground; landing gear down; power off; throttles closed; parking brake on; landing flaps up; and all doors closed. All wire assemblies shall have a unique wire number for identification purposes. This number shall follow the Aircraft manufacturer's format for identifying external (Aircraft), internal (component), twisted, shielded, and coaxial wire assemblies and shall be assigned by HI through the airline Customer. Each component shall be assigned a unique equipment designator of the format set forth by the airline Customer. All Aircraft effectivities shall be specified by assigned Aircraft registration numbers. The System wiring diagram shall be prepared and provided by HI as a Computer Aided Design (CAD) electronic file using AutoCAD 12.0, or later version, as a software design format.
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Related to AIRCRAFT SYSTEM WIRING DIAGRAM

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