P/N: 20393-000
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 20393-000 is a structural fitting machined from aerospace aluminum or steel for primary airframe load-path connections. This component reinforces fuselage frame-to-stringer joints, distributing shear and bearing loads at rivet and bolt attachment points. Installation requires specified fasteners and torque values per the aircraft Structural Repair Manual.
Used in general aviation and commercial aircraft where structural integrity and load transfer are critical to airworthiness.
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 20393-000 is a structural fitting machined from aerospace aluminum or steel for primary airframe load-path connections. This component reinforces fuselage frame-to-stringer joints, distributing shear and bearing loads at rivet and bolt attachment points.
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 20393-000.