P/N: fn212-85-322
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 |
|---|---|
| As Removed | 1 Available |
The fn212-85-322 is a structural reinforcement plate for aircraft skin and panel repairs. This aluminum doubler or splice element transfers loads around fastener rows and damaged areas, restoring structural integrity during maintenance and modification work. Installation follows FAA AC 43.13-1B sheet-metal repair guidance using AN/MS/NAS fasteners per the aircraft maintenance manual.
Commonly used in general aviation and commercial aircraft to reinforce skin panels along stress concentration points.
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 fn212-85-322 is a structural reinforcement plate for aircraft skin and panel repairs. This aluminum doubler or splice element transfers loads around fastener rows and damaged areas, restoring structural integrity during maintenance and modification work.
The PLATE 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: As Removed. 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 PLATE. 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 fn212-85-322.