P/N: an5861w2
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 AN5861W2 is a primary flight instrument that displays indicated airspeed by measuring the pressure differential between pitot and static air sources. This airspeed indicator mounts directly in the aircraft instrument panel with pneumatic connections to the pitot-static system. The dial is typically scaled in knots for general aviation use.
Certification to FAA TSO-C2 ensures accuracy and reliability for VFR and IFR operations. Installation requires proper alignment of pitot and static line connections per the aircraft maintenance manual to ensure accurate readings during flight.
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 AN5861W2 is a primary flight instrument that displays indicated airspeed by measuring the pressure differential between pitot and static air sources. This airspeed indicator mounts directly in the aircraft instrument panel with pneumatic connections to the pitot-static system.
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.