P/N: ms21044d08
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 | 2 Available |
The MS21044D08 is a self-locking hexagon nut with a nonmetallic prevailing-torque insert designed to resist vibration loosening in aircraft structures. Manufactured from aluminum alloy for weight-sensitive applications, this nut conforms to MS21044/NASM21044 specifications and accommodates 8-32 UNJC-3B threads. Rated for service temperatures to 250°F, it secures equipment brackets, panels, and structural fastening points.
Installation requires torquing per aircraft maintenance manual specifications; replace if prevailing torque falls below standard 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 MS21044D08 is a self-locking hexagon nut with a nonmetallic prevailing-torque insert designed to resist vibration loosening in aircraft structures. Manufactured from aluminum alloy for weight-sensitive applications, this nut conforms to MS21044/NASM21044 specifications and accommodates 8-32 UNJC-3B threads.
The ms21044d08 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The ms21044d08 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.