P/N: 96-520011
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The 96-520011 is a fixed rod end for aircraft trim tab control linkages. This rigid connector joins a pushrod to a bellcrank or control lever without on-aircraft adjustment capability. Machined from steel or aluminum alloy, the rod end provides a non-adjustable joint that maintains precise control geometry in trim tab actuation systems.
Installation requires torquing per the applicable aircraft maintenance manual and verification against the Illustrated Parts Catalog for compatibility with your specific airframe.
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 96-520011 is a fixed rod end for aircraft trim tab control linkages. This rigid connector joins a pushrod to a bellcrank or control lever without on-aircraft adjustment capability.
The ROD END TAB CONTRO FIXED may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: New Surplus. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the ROD END TAB CONTRO FIXED. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 96-520011.