P/N: 3071636-2
Category: Spacers & Shims
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 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.