P/N: 1213185-2
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 | 1 Available |
The 1213185-2 is a formed metal stiffener that reinforces aircraft fuselage skin and frame sections. This structural component resists local buckling under compression loads encountered during flight. Manufactured as a Textron/Cessna component, the stiffener attaches to fuselage skin bays using standard aerospace fasteners.
Installation follows aircraft maintenance manual procedures and FAA AC 43.13-1B acceptable practices. Verify compatibility with the illustrated parts catalog before installation. Proper fastening maintains structural integrity and prevents skin waviness.
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 1213185-2 is a formed metal stiffener that reinforces aircraft fuselage skin and frame sections. This structural component resists local buckling under compression loads encountered during flight.
The STIFFENER 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 STIFFENER. 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 1213185-2.