P/N: 5a16-12-27k-00-0-a
Category: Flight Computers
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 5a16-12-27k-00-0-a is an airspeed indicator that measures differential pressure between pitot and static sources to display indicated airspeed on the flight panel. This instrument connects directly to pitot and static lines and features range markings compliant with 14 CFR 23.1545. Installation and calibration must follow aircraft maintenance manual procedures to ensure accurate airspeed readout during all flight phases.
Conforms to FAA TSO-C2d standards for airspeed instruments.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 5a16-12-27k-00-0-a is an airspeed indicator that measures differential pressure between pitot and static sources to display indicated airspeed on the flight panel. This instrument connects directly to pitot and static lines and features range markings compliant with 14 CFR 23.
Avionics compatibility depends on your aircraft model and existing installation. The AIRSPEED INDICATOR is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.