P/N: 3101778-4
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 |
The 3101778-4 is a combustion chamber assembly for turbine engines, positioned between the compressor diffuser and turbine inlet. This high-temperature alloy component mixes fuel and compressed air, sustains combustion, and routes hot gases to the turbine section. Built from nickel-based superalloys, it withstands continuous operation in extreme heat environments exceeding 1,500°F.
Installation follows the applicable engine maintenance manual and Illustrated Parts Catalog specifications. Critical for maintaining combustion efficiency and turbine performance in gas turbine powerplants.
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 3101778-4 is a combustion chamber assembly for turbine engines, positioned between the compressor diffuser and turbine inlet. This high-temperature alloy component mixes fuel and compressed air, sustains combustion, and routes hot gases to the turbine section.
The 3101778-4 is currently available in the following conditions: Serviceable. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 3101778-4 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.