P/N: 45748-000
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 45748-000 is a structural plate designed for load distribution and attachment in airframe assemblies. Typically manufactured from aerospace aluminum or steel, this component functions as a doubler or mounting interface at skin, frame, or bracket connections. It spreads fastener loads across wider surface areas to reinforce repair areas or production joints.
Installation follows the applicable structural repair manual and FAA AC 43.13-1B guidance, with fit verification against the aircraft's Illustrated Parts Catalog specifications.
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 45748-000 is a structural plate designed for load distribution and attachment in airframe assemblies. Typically manufactured from aerospace aluminum or steel, this component functions as a doubler or mounting interface at skin, frame, or bracket connections.
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 45748-000.