P/N: 2111154-06
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 |
|---|---|
| Serviceable | 4 Available |
The 2111154-06 is a structural reinforcement plate for aircraft airframe assemblies. This flat bearing surface distributes fastener loads across the structure, preventing localized stress concentration at equipment-mount locations. Typically aluminum or steel construction, the plate interfaces with standard aircraft fasteners and joins brackets or fittings to the primary structure.
Installation requires fastener torque per the aircraft maintenance manual and approved engineering data. Used throughout general and commercial aircraft where structural reinforcement at attachment points is required.
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 2111154-06 is a structural reinforcement plate for aircraft airframe assemblies. This flat bearing surface distributes fastener loads across the structure, preventing localized stress concentration at equipment-mount locations.
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: Serviceable. 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 2111154-06.