P/N: 6044t41p08
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 |
|---|---|
| As Removed | 2 Available |
The 6044t41p08 is a compressor blisk (integrally bladed rotor) for gas turbine engines. This single-piece assembly integrates the rotor disk and compressor blades into one component, reducing internal leakage and part count while improving aerodynamic efficiency. Installed within axial compressor stages, the blisk must be fitted according to OEM maintenance specifications.
Verify compatibility through your aircraft's Illustrated Parts Catalog before installation. Typical material composition includes nickel-based superalloys for high-temperature strength and fatigue resistance in compressor operating conditions.
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 6044t41p08 is a compressor blisk (integrally bladed rotor) for gas turbine engines. This single-piece assembly integrates the rotor disk and compressor blades into one component, reducing internal leakage and part count while improving aerodynamic efficiency.
The 6044t41p08 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 6044t41p08 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.