PLATE (P/N 652-5-065-5) - As Removed

The 652-5-065-5 is a structural plate for aircraft fuselage assemblies. This aerospace-grade aluminum or steel component reinforces airframe loads near cutouts and fastener lines, functioning as a doubler or mounting interface. Installed using AN, MS, or NAS fasteners per approved structural drawings and aircraft maintenance manuals, the plate distributes concentrated loads across wider skin areas to prevent cracking and fatigue failure.

Common in fuselage skin repairs and reinforcement applications on general and commercial aircraft.

What is the PLATE (P/N 652-5-065-5)?

The 652-5-065-5 is a structural plate for aircraft fuselage assemblies. This aerospace-grade aluminum or steel component reinforces airframe loads near cutouts and fastener lines, functioning as a doubler or mounting interface.

Is the 652-5-065-5 a PMA or OEM part?

The PLATE 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 652-5-065-5 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 PLATE. We stock related hardware and can help identify companion parts.

Can the 652-5-065-5 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 652-5-065-5.