P/N: my20295-4017
Category: Nuts
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 | 3 Available |
The my20295-4017 is a steel lock nut designed to secure threaded assemblies against vibration in aircraft structures. This fastener uses prevailing-torque or insert locking mechanisms to maintain bolt tension during flight operations and equipment operation. Commonly installed in airframe brackets, equipment mounts, and structural connections where vibration resistance is critical.
Installation requires torquing to specification per the aircraft maintenance manual, with periodic inspection to verify prevailing torque remains within acceptable limits. Replace if locking effectiveness diminishes.
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 my20295-4017 is a steel lock nut designed to secure threaded assemblies against vibration in aircraft structures. This fastener uses prevailing-torque or insert locking mechanisms to maintain bolt tension during flight operations and equipment operation.
The my20295-4017 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The my20295-4017 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.