P/N: 137205f405
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 |
|---|---|
| New Surplus | 2 Available |
The 137205f405 is a structural plate designed for airframe load distribution and joint reinforcement. This component interfaces with MS/NAS-standard fasteners at attachment points throughout the aircraft structure. Commonly installed as a skin doubler during airframe repair to strengthen existing joints and distribute concentrated loads across larger surface areas.
Installation requires compliance with edge distance, fastener pitch, and torque specifications per the aircraft maintenance manual or FAA AC 43.13-1B guidance. Verify compatibility with the applicable Illustrated Parts Catalog 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 137205f405 is a structural plate designed for airframe load distribution and joint reinforcement. This component interfaces with MS/NAS-standard fasteners at attachment points throughout the aircraft structure.
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: New Surplus. 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 137205f405.