P/N: 3921t72p01
Category: Fasteners & Hardware
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 3 Available |
The 3921t72p01 is a self-locking nut engineered to resist vibration-induced loosening in aircraft structures. This prevailing-torque fastener maintains its grip through repeated flight cycles, eliminating the need for secondary locking devices like safety wire or cotter pins. Manufactured in aerospace-grade alloy steel, it's commonly used in airframe bracket assemblies, control linkages, and structural connections.
Install per the aircraft maintenance manual or component CMM, torquing to specification. Replace the nut if prevailing torque diminishes below acceptable limits.
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 3921t72p01 is a self-locking nut engineered to resist vibration-induced loosening in aircraft structures. This prevailing-torque fastener maintains its grip through repeated flight cycles, eliminating the need for secondary locking devices like safety wire or cotter pins.
Aircraft hardware is manufactured to military and aviation specifications. The NUT SELF LOCKING conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the 3921t72p01.
Yes, we sell hardware in various quantities from single units to bulk lots. The NUT SELF LOCKING is available in: As Removed. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.