P/N: 01261-2-14
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 01261-2-14 is a pitch computer for aircraft autopilot systems. This component generates attitude and vertical command signals that direct the pitch servo or flight director to maintain selected flight parameters. Remote-mounted within the autopilot guidance architecture, it processes sensor inputs and mode commands to stabilize pitch control during automated flight.
Installation requires verification against aircraft STC documentation and adherence to the applicable maintenance manual for proper integration with existing autopilot hardware.
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 01261-2-14 is a pitch computer for aircraft autopilot systems. This component generates attitude and vertical command signals that direct the pitch servo or flight director to maintain selected flight parameters.
Avionics compatibility depends on your aircraft model and existing installation. The PITCH COMPUTER 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.