P/N: 6053T61G03
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 | 4 Available |
| As Removed | 4 Available |
The 6053T61G03 is a stage-4 compressor stator vane sector for GE's CT7-9 turboprop engine. This component directs and diffuses compressed air between compressor rotor stages, controlling airflow entry into the downstream rotor section. The stator vane sector maintains precise blade geometry to optimize compression efficiency and engine performance.
Installation requires verification against the CT7 engine maintenance manual and aircraft IPC documentation. Commonly found in CN-235 transport aircraft and other platforms equipped with CT7-9 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 6053T61G03 is a stage-4 compressor stator vane sector for GE's CT7-9 turboprop engine. This component directs and diffuses compressed air between compressor rotor stages, controlling airflow entry into the downstream rotor section.
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 CESTOR-STG4 COMPRESSOR STATOR VANE 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 CESTOR-STG4 COMPRESSOR STATOR VANE is available in: Serviceable, As Removed. 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.