P/N: TB1015000116
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 | 2 Available |
The TB1015000116 is a metal lock plate designed to prevent fastener rotation in structural assemblies. This component pairs with bolts or nuts to maintain preload under vibration and dynamic loading. The plate's tabs bend around the fastener to create a positive lock, following FAA AC 43.13-1B safetying standards.
Commonly installed at equipment mounts, wing attachments, and control surface hinges where joint integrity is critical. Installation requires forming tabs after fastener installation and verifying fitment 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 TB1015000116 is a metal lock plate designed to prevent fastener rotation in structural assemblies. This component pairs with bolts or nuts to maintain preload under vibration and dynamic loading.
The LOCK 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 LOCK 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 TB1015000116.