CLOSE TOLERANGE BOLT (P/N 105-42110.06A1) - New Surplus

The 105-42110.06A1 is a close-tolerance bolt engineered for precision aircraft structural joints. Manufactured from aerospace-grade alloy steel, this fastener features a shank-to-hole fit designed to minimize fretting and movement in high-stress applications. Specified under NAS/MS close-tolerance fastener standards, it installs in properly reamed holes with controlled torque.

Commonly used in wing-to-fuselage attachment joints and similar critical structural connections. Verify grip length, stack-up dimensions, and installation torque in the aircraft Illustrated Parts Catalog and maintenance manual before installation.

What is the CLOSE TOLERANGE BOLT (P/N 105-42110.06A1)?

The 105-42110. 06A1 is a close-tolerance bolt engineered for precision aircraft structural joints.

What conditions is the 105-42110.06A1 available in?

The 105-42110.06A1 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.

How do I get pricing for the 105-42110.06A1?

The 105-42110.06A1 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.

Do you offer expedited shipping for the 105-42110.06A1?

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.