Overview
Cabin interior and IFE wiring runs the length of the fuselage through tight overhead and seat-track channels, so every gram and every millimeter of routing space is engineered against strict weight and certification requirements.

Design & Construction
Lightweight, Long-Run Architecture
Conductor gauge and jacket materials are selected per run to minimize weight across long cabin trunks without compromising MIL-DTL-27500 performance.
Seat & PSU Interconnect Design
Modular connector zones at each seat-track and passenger service unit position simplify cabin reconfiguration and MRO harness replacement.
Manufacturing Process
Manufactured under AS9100D quality system controls with IPC/WHMA-A-620 Class 3 workmanship and full material lot traceability from certified aerospace wire suppliers.

Typical Applications
- In-flight entertainment (IFE) system wiring
- Cabin lighting and signage harnesses
- Seat power and USB/data cabling
- Galley and lavatory equipment wiring
- Passenger service unit (PSU) interconnects
Common installations include In-flight entertainment (IFE) system wiring, Cabin lighting and signage harnesses, and Seat power and USB/data cabling, where flight-critical reliability and stringent weight optimization are the primary design drivers. The same base design can also be adapted for Galley and lavatory equipment wiring and Passenger service unit (PSU) interconnects with minor changes to connector type or cable length.
Technical Specifications
Standard configurations are available with the following technical specifications; custom configurations outside these ranges can be discussed with our engineering team. Wire Gauge: AWG 28 – 12 (MIL-spec wire). Conductor Count: 4 – 100+ circuits. Insulation: ETFE / PTFE, per MIL-DTL-27500. Temp Range: -55°C to +150°C. Voltage Rating: Up to 400V. Weight Optimization: Lightweight conductor and jacket selection for cabin runs. Workmanship: IPC/WHMA-A-620 Class 3.
Quality & Certification
AS9100D certified with AS9102 First Article Inspection available, and complete conformance documentation for airframe and cabin-retrofit programs.
Customization & Lead Time
Standard lead time for the Aircraft Cabin Interior & IFE Wiring Harness is 8–10 weeks prototype (AS9102 FAI), 4–6 weeks production. Connector type, cable length, and conductor configuration can be customized to match your exact application, including MIL-spec connector alternatives and shielding options for specific avionics or airframe integration requirements. Contact our engineering team with your drawings or requirements for a project-specific quote.
Why XinHarness
Cabin and IFE harnesses run on the same AS9100D-certified lines as our avionics and airframe programs, giving cabin integrators a single certified source for interior wiring. See the Aerospace industry page, or request a quote for your project. For related technical background, see our article on the impact of extreme temperatures on wire harness performance.
Frequently Asked Questions
All aerospace harnesses, including the Aircraft Cabin Interior & IFE Wiring Harness, are manufactured under AS9100D quality management and can be built to MIL-DTL-27500 wire and connector specifications on request.
Every Aircraft Cabin Interior & IFE Wiring Harness unit undergoes continuity, insulation resistance, and dielectric withstand testing, with additional environmental and vibration testing available for flight-critical applications.
Yes. Connector types, wire gauge, shielding, and routing length can all be customized to match your specific airframe and installation requirements — contact our engineering team with your drawings or specifications.

