P/N: 25-8wg75-1
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 |
|---|---|
| As Removed | 1 Available |
The 25-8wg75-1 is a structural reinforcement plate for aircraft fuselage assemblies. This aluminum doubler distributes fastener loads across sheet-metal joints, preventing stress concentration and skin fatigue. Installed on fuselage skins using AN/MS/NAS fasteners with proper rivet spacing and edge distance per aircraft maintenance manual specifications.
Common in general aviation and regional aircraft where skin repairs or structural reinforcement require load-sharing capability. Verify part compatibility with aircraft IPC documentation before installation.
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 25-8wg75-1 is a structural reinforcement plate for aircraft fuselage assemblies. This aluminum doubler distributes fastener loads across sheet-metal joints, preventing stress concentration and skin fatigue.
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 25-8wg75-1.