P/N: 6231276-25
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 |
Part 6231276-25 is a structural rib for aircraft wing and tailplane assemblies. This aerospace aluminum component defines airfoil contour and transfers skin and stringer loads into the main spars. The rib stabilizes wing panels, maintains camber shape, and manages fuel-bay loads during flight operations.
Installation requires fastener torque per the aircraft maintenance manual with IPC compatibility verification. Common in general aviation and commercial aircraft structures where precise aerodynamic shape and load distribution are critical.
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.
Part 6231276-25 is a structural rib for aircraft wing and tailplane assemblies. This aerospace aluminum component defines airfoil contour and transfers skin and stringer loads into the main spars.
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: 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 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 6231276-25.