P/N: sk421-67a
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 sk421-67a is a structural support bracket designed to mount and stabilize airframe members under operational loads. This component features pre-drilled or slotted holes for installation hardware, enabling secure attachment to primary and secondary airframe assemblies. Typically fabricated from aluminum or steel for weight efficiency and strength, the support maintains component positioning during flight and ground operations.
Installation follows aircraft maintenance manual specifications using standard AN/MS/NAS fasteners per FAA AC 43.13-1B guidelines.
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 sk421-67a is a structural support bracket designed to mount and stabilize airframe members under operational loads. This component features pre-drilled or slotted holes for installation hardware, enabling secure attachment to primary and secondary airframe assemblies.
The SUPPORT 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 SUPPORT. 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 sk421-67a.