P/N: M601-809.62
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 | 4 Available |
The M601-809.62 is a structural fitting designed to transfer loads between airframe members at bracketed joints. This component interfaces with standard AN/MS/NAS fasteners and maintains load path integrity at wing spar attachment points and similar critical interfaces. Installation requires the specified hardware, proper torque application, and verification against your aircraft's Illustrated Parts Catalog and maintenance manual.
Aluminum construction provides weight efficiency while meeting aerospace structural requirements.
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 M601-809. 62 is a structural fitting designed to transfer loads between airframe members at bracketed joints.
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 M601-809.62.