P/N: 6261040-12
Category: General Aircraft Parts
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 6261040-12 is a welded idler assembly that redirects control motion in aircraft flight-control linkages. This pivoting bellcrank connects cables and push-pull rods, changing direction while transmitting control input between adjacent hardware. Typically constructed from steel or aluminum, the welded assembly mounts on a bracket within the control run.
Installation and rigging must follow the aircraft maintenance manual and FAA AC 43.13-1B guidance to ensure proper alignment and control response.
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 6261040-12 is a welded idler assembly that redirects control motion in aircraft flight-control linkages. This pivoting bellcrank connects cables and push-pull rods, changing direction while transmitting control input between adjacent hardware.
The 6261040-12 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 6261040-12 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.