P/N: 360a25-1244-20z
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 | 3 Available |
The 360a25-1244-20z is a steel control rod for aircraft flight-control linkages. This component transmits push-pull motion between bellcranks and control-surface actuating arms, enabling pilot input to reach flight surfaces. Rod ends typically use SAE AS6039 (MS2115x series) connectors for secure articulation.
Installation requires rigging per the aircraft maintenance manual and verification against the Illustrated Parts Catalog to ensure correct length and alignment. Commonly found in aileron, elevator, and rudder control systems on general aviation and transport aircraft.
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 360a25-1244-20z is a steel control rod for aircraft flight-control linkages. This component transmits push-pull motion between bellcranks and control-surface actuating arms, enabling pilot input to reach flight surfaces.
The ROD 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. 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 360a25-1244-20z.