P/N: 3071636-2
Category: Spacers & Shims
Flat-rate shipping. Choose Ground or a faster service at checkout.
Flat-rate shipping covers most parts. If your order turns out to need freight or special handling, we'll contact you with the updated shipping cost before it ships. You can pay the difference or cancel for a full refund. International buyers pay any duties and import taxes.
| Condition | Price | Stock |
|---|---|---|
| New Surplus | $18.00 | 29 Available |
The 3071636-2 is a high-temperature alloy spacer for turbine nozzle assemblies in gas turbine engines. This component positions between nozzle segments to maintain precise axial stack height and vane ring alignment within the hot-section assembly. The spacer controls critical clearances during engine build and operation, ensuring proper nozzle geometry and flow characteristics.
Installation occurs during hot-section maintenance per engine maintenance manual specifications. Verify part compatibility with the Illustrated Parts Catalog before assembly.
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 3071636-2 is a high-temperature alloy spacer for turbine nozzle assemblies in gas turbine engines. This component positions between nozzle segments to maintain precise axial stack height and vane ring alignment within the hot-section assembly.
The 3071636-2 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 3071636-2 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.