P/N: 1221042-98
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 | 1 Available |
The 1221042-98 is a structural rib for Cessna aircraft wing and tail assemblies. This component maintains airfoil geometry and transfers aerodynamic skin loads to the primary spars and stringers. Ribs are installed perpendicular to spars within the wing box or control-surface structure using approved fasteners.
Installation requires torquing to specification per the aircraft maintenance manual and verifying compatibility with the illustrated parts catalog. Aluminum construction provides strength-to-weight efficiency typical of general aviation airframe design.
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 1221042-98 is a structural rib for Cessna aircraft wing and tail assemblies. This component maintains airfoil geometry and transfers aerodynamic skin loads to the primary spars and stringers.
The RIB 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. 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 RIB. 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 1221042-98.