P/N: as-391a
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 | 2 Available |
The as-391a is an airspeed indicator that measures and displays indicated airspeed on the aircraft instrument panel. It receives pressure differential data from pitot and static lines, converting this input into precise airspeed readings. The instrument connects directly to approved pitot-static system tubing and requires periodic certification under 14 CFR Part 91.411 pitot-static checks.
Installation follows the aircraft maintenance manual with proper line connections and panel mounting. Essential for flight operations, this indicator provides real-time airspeed data for safe takeoff, cruise, and landing performance.
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 as-391a is an airspeed indicator that measures and displays indicated airspeed on the aircraft instrument panel. It receives pressure differential data from pitot and static lines, converting this input into precise airspeed readings.
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.