P/N: 6044t42p08
Category: Pneumatic Components
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 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.
Hydraulic component compatibility depends on the aircraft system design. Common aviation hydraulic fluids include MIL-PRF-5606 (mineral-based), MIL-PRF-83282 (synthetic), and Skydrol (phosphate ester). Verify the BLADE DISK STG 5 COMPRESSOR against your aircraft maintenance manual for fluid compatibility.
Overhauled and repaired hydraulic components are pressure-tested per manufacturer specifications and include 8130-3 documentation. The BLADE DISK STG 5 COMPRESSOR is available in: Serviceable. Contact us for test documentation on your selected condition.
In-stock hydraulic components ship same business day before 3 PM EST. We provide 24/7 AOG support at (904) 998-9101 for urgent hydraulic system needs. RFQ submissions are typically quoted within 24 hours.