P/N: 2111314-4
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 |
|---|---|
| New Surplus | 1 Available |
The 2111314-4 is an aerospace-grade metal structural support designed for fuselage frame subassemblies. This component provides local reinforcement and load transfer, maintaining alignment between adjacent structural members. Installed within panel stiffening applications, the support transfers flight loads and pressurization forces to the primary structure.
Installation requires aerospace-standard hardware with torque values specified in the aircraft maintenance manual. Verify part number against the Illustrated Parts Catalog before installation to ensure correct application and compatibility with your airframe.
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 2111314-4 is an aerospace-grade metal structural support designed for fuselage frame subassemblies. This component provides local reinforcement and load transfer, maintaining alignment between adjacent structural members.
The SUPPORT 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 SUPPORT. 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 2111314-4.