FITTING (P/N my20164-70) - New Surplus

The MY20164-70 is a metal structural fitting designed to join and support aircraft airframe members at critical load points. This component transfers structural loads between fuselage, wing, or empennage sections while maintaining alignment and integrity. Manufactured to OEM specifications and MS/NAS hardware standards, the fitting accommodates bolted or riveted assembly methods.

Verify applicability in your aircraft's Illustrated Parts Catalog before installation. Follow the applicable Structural Repair Manual for torque specifications, fastener selection, and inspection requirements.

What is the FITTING (P/N my20164-70)?

The MY20164-70 is a metal structural fitting designed to join and support aircraft airframe members at critical load points. This component transfers structural loads between fuselage, wing, or empennage sections while maintaining alignment and integrity.

Is the my20164-70 a PMA or OEM part?

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.

Does the my20164-70 include installation hardware?

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.

Can the my20164-70 be shipped internationally?

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 my20164-70.