LEVER (P/N 25um1084a) - As Removed

The 25um1084a is a mechanical control lever for aircraft linkage assemblies. This component translates input motion through a pivot point to actuate connected rods or cables in valve and mechanism control systems. Typically fabricated from aluminum or steel, the lever integrates with standard aerospace hardware following AN, MS, or NAS fastener conventions.

Installation requires verification against the aircraft's Illustrated Parts Catalog and adherence to the applicable maintenance manual procedures, including proper safetying of attachment hardware.

What is the LEVER (P/N 25um1084a)?

The 25um1084a is a mechanical control lever for aircraft linkage assemblies. This component translates input motion through a pivot point to actuate connected rods or cables in valve and mechanism control systems.

Is the 25um1084a a PMA or OEM part?

The LEVER 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.

Does the 25um1084a include installation hardware?

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 LEVER. We stock related hardware and can help identify companion parts.

Can the 25um1084a be shipped internationally?

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 25um1084a.