P/N: 409it07p02
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 |
|---|---|
| Serviceable | 1 Available |
The 409it07p02 is a stage 4 turbine ring for gas turbine engines, providing flow-path shrouding and tip-clearance control at the fourth turbine stage. Manufactured from high-temperature alloy materials, this hot-section component withstands extreme thermal and mechanical stresses during engine operation. Installed within the turbine module during engine overhaul and maintenance.
Assembly must follow the engine manufacturer's maintenance manual and comply with FAA 14 CFR Part 43 requirements. Verify applicability and proper fit before installation.
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 409it07p02 is a stage 4 turbine ring for gas turbine engines, providing flow-path shrouding and tip-clearance control at the fourth turbine stage. Manufactured from high-temperature alloy materials, this hot-section component withstands extreme thermal and mechanical stresses during engine operation.
The 409it07p02 is currently available in the following conditions: Serviceable. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 409it07p02 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.