P/N: c6fs1623-61
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 | 8 Available |
The c6fs1623-61 is a structural reinforcement plate designed for load transfer and fatigue resistance at fuselage skin joints. This metal component functions as a doubler or splice, spreading fastener loads across a wider area to prevent stress concentration and cracking. Manufactured to engineering specifications, it's installed with approved fasteners and torqued per aircraft maintenance manual requirements.
Verify part compatibility in the 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 c6fs1623-61 is a structural reinforcement plate designed for load transfer and fatigue resistance at fuselage skin joints. This metal component functions as a doubler or splice, spreading fastener loads across a wider area to prevent stress concentration and cracking.
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 c6fs1623-61.