P/N: 2453025-1
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 | 1 Available |
The 2453025-1 is a structural doubler—a reinforcement plate that strengthens stressed-skin aircraft assemblies. Typically fabricated from aluminum sheet metal, it bridges loads across repairs and distributes stress around access openings to arrest crack growth. Riveted to the primary structure, the doubler maintains continuous load paths and adds local thickness where structural integrity is critical.
Install per the applicable Structural Repair Manual or FAA AC 43.13-1B guidance. Common in fuselage, wing, and empennage repairs on general aviation and commercial aircraft.
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 2453025-1 is a structural doubler—a reinforcement plate that strengthens stressed-skin aircraft assemblies. Typically fabricated from aluminum sheet metal, it bridges loads across repairs and distributes stress around access openings to arrest crack growth.
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 2453025-1.