P/N: 0516023-4
Category: Structural Components
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 0516023-4 is a structural fitting designed to join and reinforce airframe members in load-bearing assemblies. This Cessna OEM component connects critical junction points such as bracket-to-spar interfaces where structural loads concentrate. Typically fabricated from aluminum alloy or steel to withstand flight and ground stresses.
Installation requires verification against your aircraft's Illustrated Parts Catalog and adherence to the applicable maintenance manual procedures. Proper alignment and fastener torque are essential for maintaining airframe integrity.
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 0516023-4 is a structural fitting designed to join and reinforce airframe members in load-bearing assemblies. This Cessna OEM component connects critical junction points such as bracket-to-spar interfaces where structural loads concentrate.
The FITTING 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.
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 FITTING. 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 0516023-4.