The Power Supply is based on a modular concept. The Power Supply is a basic element of the PAXCOM system. For further information please have a look on the Power Supply sub-page.

Technical data:

  • 115V AC WF power input
  • up to 300W output
  • low standy by current
  • quick lock plugs
  • modular system / flexible Interface Box
  • weight ~ 600 g / ~ 1,32 lb (Power Supply olny)
  • fan-less cooling

Compliance:

Airbus:

  • 2520M1F001200, Electrical Seat Actuation System, Issue 2
  • ABD0100, Equipment Design – General Requirements for Suppliers, Issue G
  • ABD0031, Fire Worthiness Requirements - Pressurized Section of Fuselage, Issue E

Boeing:

  • D6-36440, Standard Cabin System Requirements Document, Rev. G
  • D6-44588, Electrical Requirements for Utilization Equipment Installed on
  • Commercial Transport Airplanes, Rev. AA
  • D6-51377, Airplane Fire Worthiness Design Criteria - Pressurized Compartments, Rev. F

Others:

  • RTCA/DO160G, Environmental Conditions and Test Procedures for Airborne Equipment
  • RTCA/DO178B, Software Considerations in Airborne Systems and Equipment Certification

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The PAXCOM development (except the power supply) is supported through the Federal Ministry for Economic Affairs and Energy.

  

Please contact us

Werner Berlage
Commercial Director and Sales

» write an email
Phone 00 49 7556 9225 0