P/N: 0841111-3
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 0841111-3 is a Cessna OEM structural fitting designed to join and terminate airframe members at critical attachment points. This machined metal end fitting transfers loads between primary and secondary structural components in the fuselage, wings, or empennage. Installation requires torque verification per the aircraft maintenance manual and SRM specifications.
Verify part applicability in the Illustrated Parts Catalog before replacement to ensure correct load path and structural integrity during flight operations.
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 0841111-3 is a Cessna OEM structural fitting designed to join and terminate airframe members at critical attachment points. This machined metal end fitting transfers loads between primary and secondary structural components in the fuselage, wings, or empennage.
The FITTING 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 FITTING. 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 0841111-3.