BOLT (P/N 212-42000-10-1) - New Surplus, As Removed

The 212-42000-10-1 is an aircraft structural bolt conforming to AN/MS/NAS aerospace fastener standards. This steel bolt transfers loads in airframe assemblies, fuselage joints, and system component mounting points. Installation requires matching washers, a self-locking nut, and torque application per aircraft maintenance manual specifications.

Verify diameter, grip length, and thread type against the Illustrated Parts Catalog before assembly. Proper fastener selection and installation ensure structural integrity and load-bearing reliability in critical aircraft joints.

What is the BOLT (P/N 212-42000-10-1)?

The 212-42000-10-1 is an aircraft structural bolt conforming to AN/MS/NAS aerospace fastener standards. This steel bolt transfers loads in airframe assemblies, fuselage joints, and system component mounting points.

Does the 212-42000-10-1 meet AN/MS/NAS aviation specifications?

Aircraft hardware is manufactured to military and aviation specifications. The BOLT conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.

What material is the 212-42000-10-1 manufactured from?

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 212-42000-10-1.

Can I order the 212-42000-10-1 in custom quantities?

Yes, we sell hardware in various quantities from single units to bulk lots. The BOLT is available in: New Surplus, As Removed. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.