P/N: 0523003-11
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 0523003-11 is an OEM Cessna aluminum airframe skin panel for semi-monocoque fuselage and wing structures. This stressed-skin component restores aerodynamic surface continuity and carries primary bending loads as part of the airframe load path. Replaces damaged or corroded skin sections on Cessna aircraft.
Installation requires alignment with existing structure, fastener hole matching, and adherence to the Structural Repair Manual and FAA AC 43.13-1B guidance. Verify part compatibility with your specific aircraft model using the Illustrated Parts Catalog before ordering.
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 0523003-11 is an OEM Cessna aluminum airframe skin panel for semi-monocoque fuselage and wing structures. This stressed-skin component restores aerodynamic surface continuity and carries primary bending loads as part of the airframe load path.
The SKIN 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 SKIN. 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 0523003-11.