P/N: 74-10
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 74-10 is a metal backing plate for aircraft structural reinforcement. This component distributes fastener and rivet loads across a wider bearing area, preventing skin deformation during panel and bracket attachments. Installed behind sheet-metal joints during airframe repairs, the plate back supports fastener loads while maintaining structural integrity.
Used in general aviation and commercial aircraft maintenance to reinforce attachment points on fuselage panels, control surfaces, and access covers. Installation follows aircraft Structural Repair Manual specifications and FAA AC 43.13-1B accepted practices.
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 74-10 is a metal backing plate for aircraft structural reinforcement. This component distributes fastener and rivet loads across a wider bearing area, preventing skin deformation during panel and bracket attachments.
The PLATE BACK 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 BACK. 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 74-10.