ROCTEXOAEROSPACE
RX1-10-07493

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RX1-10-07493

Mid-Continent Instruments and Avionics Max Power USB Charging Port 15With 3A And 100With 5A Out Per Port 22-32 VDC In Dual USB-A/USB-C Pd Rear Connector Lighted

588.94 EUR/EA

Excluding VAT

Availability

Up to 7 EA ready to ship on Thursday 2026-11-12Order before 16:00 CET Today
Up to 9 EA ready to ship on Monday 2026-11-16Order before 16:00 CET Today
12 EA available on request, inbound freight fee of 60 EUR appliesSpecial order from vendor stock.

Part numbers

Roctexo
RX1-10-07493
Manufacturer
6430360-31
Vendor
10-07493

Product details

The True Blue Power TA360-CAL MAX Power USB Charging Port, manufacturer part number 6430360-31, is a lighted dual-port aircraft USB charging solution from Mid-Continent Instruments and Avionics. It combines one USB Type-A port with one USB Type-C Power Delivery (PD) port in a compact, rear-connector panel-mount unit.

The USB-C PD port uses intelligent device negotiation to provide the appropriate charging voltage for compatible equipment, while the USB-A port supports conventional USB charging. Integrated illumination assists port location in low-light cabin or cockpit environments.

  • Manufacturer part number: 6430360-31
  • Model: TA360-CAL MAX Power USB Charging Port
  • Input: 22–32 VDC
  • USB-C PD output: up to 100 W and 5 A; auto-adjustable 5, 9, 15 or 20 VDC
  • USB-A output: up to 15 W and 3 A at 5 VDC
  • Dual USB Type-A and USB Type-C PD configuration
  • Lighted charging ports
  • Rear connector and rear panel-mount installation
  • Approximate unit dimensions, excluding mating connector: 38 × 26 × 50 mm
  • Built-in protection for over-current, short circuit, low input voltage, over-temperature and reverse-polarity installation
  • FAA TSO-C71 certified; qualified to RTCA DO-160G environmental conditions

A mating power connector kit and mounting screws are identified in the manufacturer’s installation documentation. The manufacturer recommends thermal management consideration for 100 W versions operating continuously at high power. Aircraft installation must be evaluated and approved as applicable to the specific installation and airworthiness requirements.

Relevant documentation: TA360 Series Installation Manual and Operating Instructions.