P/N: 3102102-3
Category: General Aircraft Parts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
| Overhauled | 1 Available |
The 3102102-3 is a nickel alloy transition liner assembly for Honeywell T76-G-420/421 turbine engines. This component channels hot combustor gases into the turbine section, managing thermal flow between engine stages. Fabricated from AMS5536 nickel alloy to withstand extreme combustor temperatures and pressure differentials.
Installation follows the applicable Honeywell engine maintenance manual with applicability verification through the engine illustrated parts catalog. NSN 2840-01-245-8118.
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 3102102-3 is a nickel alloy transition liner assembly for Honeywell T76-G-420/421 turbine engines. This component channels hot combustor gases into the turbine section, managing thermal flow between engine stages.
The 3102102-3 is currently available in the following conditions: Serviceable, Overhauled. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 3102102-3 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.