P/N: 65-59316-212
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 | 2 Available |
The 65-59316-212 is an extruded aluminum structural angle for aircraft airframe reinforcement. This L-shaped profile joins and stiffens fuselage, wing, and tail members at panel and frame interfaces. The angle distributes concentrated loads across structural connections while preventing edge buckling in high-stress areas.
Installation uses approved fasteners per the aircraft maintenance manual and FAA AC 43.13-1B guidelines. Verify part compatibility with your aircraft's Illustrated Parts Catalog before installation.
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 65-59316-212 is an extruded aluminum structural angle for aircraft airframe reinforcement. This L-shaped profile joins and stiffens fuselage, wing, and tail members at panel and frame interfaces.
The ANGLE 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 ANGLE. 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 65-59316-212.