FRAME (P/N 105-530011-3) - As Removed

The 105-530011-3 is a structural frame subassembly that provides local support within aircraft fuselage or cabin bays. This component mounts interior panels, system brackets, and equipment while maintaining structural integrity of the airframe. Typically fabricated from aluminum or steel, the frame integrates with existing fuselage structure through fastener interfaces.

Installation requires verification against the aircraft's Illustrated Parts Catalog and compliance with the applicable maintenance manual. Minor repairs follow FAA AC 43.13-1B acceptable methods.

What is the FRAME (P/N 105-530011-3)?

The 105-530011-3 is a structural frame subassembly that provides local support within aircraft fuselage or cabin bays. This component mounts interior panels, system brackets, and equipment while maintaining structural integrity of the airframe.

Is the 105-530011-3 a PMA or OEM part?

The FRAME 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 105-530011-3 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 FRAME. We stock related hardware and can help identify companion parts.

Can the 105-530011-3 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 105-530011-3.