P/N: 6044t42p08
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 6044t42p08 is a stage-5 compressor rotor blade disk for General Electric CT7-5 and CT7-7 turboshaft engines. This titanium alloy component compresses incoming air within the engine core during the fifth compression stage. The blade disk integrates with the compressor rotor assembly (NHA 6080T53G01) and requires precise balance verification during installation per GE maintenance specifications.
NSN 2840-01-495-3511 identifies this critical engine component for airworthiness traceability and MRO documentation.
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 6044t42p08 is a stage-5 compressor rotor blade disk for General Electric CT7-5 and CT7-7 turboshaft engines. This titanium alloy component compresses incoming air within the engine core during the fifth compression stage.
The 6044t42p08 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 6044t42p08 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.