P/N: 212-961-051-043
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 |
Part 212-961-051-043 is a structural doubler plate designed to reinforce aircraft skin and panel areas around cutouts, access openings, and fastener rows. This aluminum component improves load distribution and fatigue resistance by backing up stress concentration points. Installed during maintenance or structural modifications using approved fastener patterns and edge distances per AC 43.13-1B guidance.
The doubler bonds or fastens to existing structure using AN/MS hardware, extending the service life of reinforced sections.
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.
Part 212-961-051-043 is a structural doubler plate designed to reinforce aircraft skin and panel areas around cutouts, access openings, and fastener rows. This aluminum component improves load distribution and fatigue resistance by backing up stress concentration points.
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 212-961-051-043.