P/N: 4881
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 |
|---|---|
| As Removed | 1 Available |
The 4881 is a cable assembly for aircraft control systems that transmits cockpit inputs to control surfaces via tensioned wire rope. This flexible cable connects pilot pedals to the rudder bellcrank, converting foot pressure into directional control movement. Constructed with wire rope per MIL-DTL-83420 and swaged terminals per MIL-DTL-781 for reliable load transfer.
Installation requires routing through cable guides while maintaining proper tension and verifying terminal security per the aircraft maintenance manual. Used in general aviation and light aircraft rudder control runs.
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 4881 is a cable assembly for aircraft control systems that transmits cockpit inputs to control surfaces via tensioned wire rope. This flexible cable connects pilot pedals to the rudder bellcrank, converting foot pressure into directional control movement.
The CABLE ASSY 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: As Removed. 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 CABLE ASSY. 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 4881.