P/N: 5011023-2
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 | 2 Available |
The 5011023-2 is a structural fitting designed to transfer loads between airframe members in aircraft assemblies. Machined from aluminum or steel, this component provides rigid connection points for bulkhead attachments and primary structure interfaces. Installation requires approved AN/MS/NAS fasteners per aircraft maintenance manual specifications.
Verify part number against the Illustrated Parts Catalog before installation to ensure compatibility with your airframe assembly. The fitting maintains load-bearing integrity under flight and ground operational stresses.
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 5011023-2 is a structural fitting designed to transfer loads between airframe members in aircraft assemblies. Machined from aluminum or steel, this component provides rigid connection points for bulkhead attachments and primary structure interfaces.
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 5011023-2.