P/N: 212-41206.5
Category: Bolts
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| Condition | Price | Stock |
|---|---|---|
| New Surplus | $625.00 | 2 Available |
The 212-41206.5 is an alloy steel aircraft bolt designed for structural and system component fastening under tension and shear loads. This fastener conforms to AN/MS/NAS standards for dimensions, threading, and material specifications. Common applications include airframe bracket assemblies, control surface attachments, and landing gear installations where reliable load-bearing connections are required.
Installation requires verification of grip length, proper nut and washer selection, and torque application per the aircraft maintenance manual and FAA AC 43.13-1B guidance.
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 212-41206. 5 is an alloy steel aircraft bolt designed for structural and system component fastening under tension and shear loads.
The 212-41206.5 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-41206.5 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.