Overview
Landing gear bays subject wiring to repeated mechanical shock, hydraulic fluid exposure, and extreme temperature swings between ground and altitude, all while requiring precise sensor feedback for safe gear operation.
Design & Construction
Shock & Vibration-Rated Construction
Reinforced strain relief and vibration-rated clamping withstand the repeated mechanical shock of gear retraction and extension cycles, protecting sensor and actuator circuits over the airframe’s service life.
Hydraulic Fluid & Temperature-Resistant Sealing
Fluid-resistant overbraid and sealed circular connectors protect position sensor and actuator wiring from hydraulic fluid exposure and the wide temperature swings seen in wheel well environments.
Manufacturing Process
Built under AS9100D quality management with full first-article inspection and lot traceability, supporting landing gear OEMs and MRO providers on both new-build and retrofit programs.
Typical Applications
- Landing gear position sensor wiring
- Brake and anti-skid system cabling
- Actuator control and feedback harnesses
- Wheel well lighting and de-icing circuits
- Gear retraction/extension monitoring wiring
Common installations include Landing gear position sensor wiring, Brake and anti-skid system cabling, and Actuator control and feedback harnesses, where flight-critical reliability and stringent weight optimization are the primary design drivers. The same base design can also be adapted for Wheel well lighting and de-icing circuits and Gear retraction/extension monitoring wiring 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 26 – 12. Conductor Count: 4 – 44 circuits. Insulation: Fluid-resistant, high-temp rated. Temp Range: -55°C to +200°C. Fluid Resistance: Hydraulic fluid and de-icing fluid rated. Shock Rating: Vibration and mechanical shock tested. Connector Standard: Sealed circular, MIL-spec.
Quality & Certification
Manufactured under AS9100D and ISO 9001 certification, with material and process traceability documentation suitable for landing gear system airworthiness certification.
Customization & Lead Time
Standard lead time for the Aircraft Landing Gear & Actuation Wiring Harness is 6–8 weeks prototype, 3–4 weeks production reorder. 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
Landing gear and actuation harnesses run on the same AS9100D-certified lines as our avionics and engine programs, giving gear system integrators a single certified source for flight-critical 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 Landing Gear & Actuation Wiring Harness, are manufactured under AS9100D quality management and can be built to MIL-DTL-27500 wire and connector specifications on request.
Every Aircraft Landing Gear & Actuation 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.
