BOLT (P/N 212-42000-10-1) - New Surplus, As Removed
P/N: 212-42000-10-1
Category: Bolts
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Available Inventory
| Condition | Price | Stock |
|---|---|---|
| New Surplus | $995.00 | 21 Available |
| As Removed | $995.00 | 3 Available |
Product Description
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.
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.
Frequently Asked Questions
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.
What conditions is the 212-42000-10-1 available in?
The 212-42000-10-1 is currently available in the following conditions: New Surplus, As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 212-42000-10-1?
The 212-42000-10-1 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.
Do you offer expedited shipping for the 212-42000-10-1?
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.
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