P/N: f20g8021195-6
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 |
|---|---|
| New Surplus | 1 Available |
The f20g8021195-6 is a metal structural fitting designed to join airframe members while carrying shear and tensile loads. This component interfaces at fuselage frame-to-stringer connections, providing critical load transfer in aircraft structure. Installation follows aerospace fastening practices with approved fastener types, proper edge distances, and engineering-verified torque specifications.
Compatible with standard aircraft structural repair procedures and maintenance protocols for general and commercial aviation.
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 f20g8021195-6 is a metal structural fitting designed to join airframe members while carrying shear and tensile loads. This component interfaces at fuselage frame-to-stringer connections, providing critical load transfer in aircraft structure.
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: New Surplus. 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 f20g8021195-6.