P/N: 2121021-11
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 2121021-11 is an aerospace aluminum structural rib that maintains airfoil geometry within wing assemblies. This component transfers loads from the wing skin and stringers to the main spars, preventing buckling under flight stresses. Installed perpendicular to spars using aircraft-specific fastener patterns, the rib provides shape control and lateral bracing throughout the wing structure.
Installation follows the applicable Structural Repair Manual with specified torque and alignment procedures. Common on general and commercial aircraft wings requiring load distribution and geometric stability.
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 2121021-11 is an aerospace aluminum structural rib that maintains airfoil geometry within wing assemblies. This component transfers loads from the wing skin and stringers to the main spars, preventing buckling under flight stresses.
The RIB 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 RIB. 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 2121021-11.