P/N: ms2104216
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 | 7 Available |
The MS21042/16 is an all-metal prevailing-torque hex nut with reduced height, manufactured from steel to MS21042/NASM21042 specifications. This self-locking nut resists vibration loosening in aircraft structural fastening applications. Install with UNJF or UNF bolts in access panel installations and vibration-prone locations.
The prevailing torque mechanism maintains bolt tension without additional locking devices, meeting aerospace vibration resistance requirements. Verify the correct dash size in the aircraft IPC 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 MS21042/16 is an all-metal prevailing-torque hex nut with reduced height, manufactured from steel to MS21042/NASM21042 specifications. This self-locking nut resists vibration loosening in aircraft structural fastening applications.
The ms2104216 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The ms2104216 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.