P/N: 212-42000-07.1
Category: Bolts
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| Condition | Price | Stock |
|---|---|---|
| New Surplus | $250.00 | 1 Available |
The 212-42000-07.1 is a hex head bolt for aircraft structural fastening. This alloy steel fastener provides secure clamping of brackets, housings, and components where wrench access permits installation. The bolt pairs with matching nuts or self-locking nuts to create reliable joints in airframe assemblies.
Torque specifications follow FAA AC 43.13-1B and the applicable aircraft maintenance manual. Conforms to AN, MS, or NAS standards typical of aviation hardware applications. Used throughout general and commercial aircraft for primary and secondary structure attachment.
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 212-42000-07. 1 is a hex head bolt for aircraft structural fastening.
The 212-42000-07.1 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-42000-07.1 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.