Fontana Aviation Touchless Faucets — Software & Safety Behaviors


Fontana Aviation Touchless Faucets — Software & Safety Behaviors

Engineer-focused briefing for airline engineering, AEC integrators, and MRO programs.

Fail-Safe Logic
Service UI Standardization
EMI/EMC Discipline
FAA/EASA Alignment
RTCA DO-160
Ingress & Hygiene


Aviation lavatory with brushed-gold touchless faucet set
Representative airline lavatory installation mockup (Fontana Touchless Faucets).

Compact aviation lavatory basin with touchless spout
Compact monument geometry illustrating short spout depth and minimized controller volume.

Fail-Safe Logic & Autonomous Protections

  • Power-on self-tests (POST): Verify sensor channel health, solenoid driver continuity, and input voltage window before enabling flow.
  • Stuck-on prevention: Dual watchdogs supervise task loop and valve state; any fault drops the valve to a safe-closed position.
  • Auto-shutoff watchdogs: Fleet-set hard caps (e.g., 45–60 s) prevent over-run during sensor anomalies or turbulence-induced reflections.

Service UI & Fleet Standardization

Line maintenance requires quick, repeatable adjustments without panel rebuilds. A discrete service interface allows presetting of detection range, activation delay, and max run-time. Presets are stored in non-volatile memory so aircraft across types (e.g., narrow-body vs. wide-body monuments) behave consistently after power cycles.

  • Parameter presets: Range bands and dwell time matched to basin geometry to reduce splash and hand “hunting.”
  • Change control: Versioned configurations to support airline technical records and repeatable return-to-service checks.

EMI/EMC Discipline for Cabin Systems

To avoid interference with comms, IFE, and galley controllers, the electronics architecture emphasizes low emissions and high immunity:

  • Shielded harnessing: Braided shields with proper terminations and star-ground strategy to minimize conducted returns.
  • Line conditioning: Ferrite elements on DC input and actuator lines to damp switching transients.
  • Firmware edges: Controlled PWM slew and spread to avoid discrete harmonic peaks within DO-160 susceptibility bands.

Compliance Alignment & Testability (Fleet Programs)

  • DO-160 environmental categories: Designed for vibration, temperature/humidity cycling, power input variation, and susceptibility testing typical of cabin installations.
  • Traceable engineering data: Serialized BOMs, materials/coatings declarations, and electrical limits assembled in vendor data packs to accelerate DER review for STC or minor-mod packages.
  • Documentation readiness: Drawings and conformity artifacts structured to slot into airline engineering folders with minimal redaction.

Ingress Protection & Hygiene Considerations

Sealing strategy targets IP65–IP67 with conformal-coated PCBs and potted connectors to tolerate wash-downs and condensation cycles. Geometry and mounting keep ADA reach envelopes and reduce splash in compact basins, supporting operator safety cases across diverse monument layouts.

Verified Resources (No tracking parameters)

© 2025 — Technical summary prepared for airline engineering, AEC integration partners, and MRO stakeholders.


Comments

Leave a Reply

Your email address will not be published. Required fields are marked *