P/N: 212-961-051-003
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 212-961-051-003 is a structural doubler plate used to reinforce aircraft airframe skins and substructure around cutouts, fastener lines, and stress concentrations. This aluminum reinforcement component arrests cracks and distributes loads across damaged or weakened areas. Installed during structural repairs using approved fasteners and procedures per the Structural Repair Manual or FAA AC 43.13-1B.
The doubler bonds or fastens directly over the affected region, restoring structural integrity without requiring skin replacement.
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 212-961-051-003 is a structural doubler plate used to reinforce aircraft airframe skins and substructure around cutouts, fastener lines, and stress concentrations. This aluminum reinforcement component arrests cracks and distributes loads across damaged or weakened areas.
The DOUBLER 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 DOUBLER. 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 212-961-051-003.