P/N: 3101524-5
Category: Turbine Engine Parts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 3101524-5 is a combustor transition liner for turbine engines, channeling high-temperature combustion gases from the combustor into the turbine inlet section. Manufactured from oxidation-resistant superalloy, this component smooths gas flow and conditions hot exhaust toward the nozzle guide vanes. Installed in the engine's combustion section, it withstands extreme heat and pressure during operation.
Service and installation follow the applicable engine maintenance manual and FAA Part 43 authorized procedures. Critical for maintaining efficient turbine inlet conditions and engine performance.
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 3101524-5 is a combustor transition liner for turbine engines, channeling high-temperature combustion gases from the combustor into the turbine inlet section. Manufactured from oxidation-resistant superalloy, this component smooths gas flow and conditions hot exhaust toward the nozzle guide vanes.
The 3101524-5 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 3101524-5 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.