P/N: 1379530h3
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 | 4 Available |
The 1379530h3 is a structural reinforcement plate designed to distribute loads and strengthen joints in aircraft structures. Fabricated from aircraft-grade aluminum, this plate functions as a mounting doubler or repair reinforcement at cutouts, hinges, and system attachment points. It mates with MS/NAS fasteners and installs using approved hardware with torque specifications per the aircraft structural repair manual.
Common in general and commercial aviation for wing-to-fuselage connections, control surface hinges, and equipment mounting locations.
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 1379530h3 is a structural reinforcement plate designed to distribute loads and strengthen joints in aircraft structures. Fabricated from aircraft-grade aluminum, this plate functions as a mounting doubler or repair reinforcement at cutouts, hinges, and system attachment points.
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 1379530h3.