P/N: 35641-008
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 35641-008 is an aircraft stiffener for reinforcing wing skin panels and airframe assemblies. This formed aluminum component improves structural rigidity and distributes aerodynamic loads across the skin between ribs. Secured with riveted attachments following OEM specifications, the stiffener prevents skin buckling and maintains panel flatness during flight operations.
Installation requires verification of part-number compatibility and fastener pattern per the aircraft Structural Repair Manual and Illustrated Parts Catalog during MRO maintenance.
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 35641-008 is an aircraft stiffener for reinforcing wing skin panels and airframe assemblies. This formed aluminum component improves structural rigidity and distributes aerodynamic loads across the skin between ribs.
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: 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 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 35641-008.