P/N: 1211658-1
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 | 2 Available |
Part 1211658-1 is a structural reinforcement plate for aircraft airframe assemblies. This flat load-spreading member installs around access-panel openings to distribute fastener loads and prevent stress concentration in the fuselage skin. Fabricated from aerospace-grade aluminum or steel stock, the plate mounts using standard AN/MS/NAS fasteners per aircraft maintenance manual specifications.
Installation follows FAA AC 43.13-1B accepted practices and requires verification against the applicable Illustrated Parts Catalog for 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.
Part 1211658-1 is a structural reinforcement plate for aircraft airframe assemblies. This flat load-spreading member installs around access-panel openings to distribute fastener loads and prevent stress concentration in the fuselage skin.
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: 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 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 1211658-1.