P/N: 270-0859-010
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 |
|---|---|
| Serviceable | 1 Available |
The 270-0859-010 is an altitude control component for aircraft autopilot systems, manufactured by Rockwell Collins. This control unit provides command input for altitude capture and hold functions within the flight control electronics. Installed on autopilot control panels, it allows pilots to set and maintain desired altitude automatically.
The component follows NSN 6615-01-227-4279 specifications. Installation and operational verification must be performed by qualified avionics personnel per the aircraft maintenance manual and autopilot manufacturer documentation.
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 270-0859-010 is an altitude control component for aircraft autopilot systems, manufactured by Rockwell Collins. This control unit provides command input for altitude capture and hold functions within the flight control electronics.
The ALTITIUDE CONTROL 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: Serviceable. 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 ALTITIUDE CONTROL. 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 270-0859-010.