STUD (P/N 31c17p03) - New Surplus
P/N: 31c17p03
Category: Fasteners & Hardware
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| New Surplus | 9 Available |
Product Description
The 31c17p03 is a threaded stud for Lycoming engine assemblies, sized.3125-18 x 2.13 inches long. This fastener provides a secure attachment point for engine components in powerplant installations. The stud threads into engine bosses and accepts nuts or other fasteners to clamp assemblies during both production and maintenance operations.
Installation requires correct thread engagement and torque specifications per Lycoming maintenance documentation. Commonly used in MRO settings for engine teardown, reassembly, and component replacement on Lycoming-powered aircraft.
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 STUD (P/N 31c17p03)?
The 31c17p03 is a threaded stud for Lycoming engine assemblies, sized. 3125-18 x 2.
Does the 31c17p03 meet AN/MS/NAS aviation specifications?
Aircraft hardware is manufactured to military and aviation specifications. The STUD 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 31c17p03 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 31c17p03.
Can I order the 31c17p03 in custom quantities?
Yes, we sell hardware in various quantities from single units to bulk lots. The STUD is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.