P/N: 3075584-16
Category: Fuel Nozzles
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 3075584-16 is a cooled high-pressure turbine nozzle segment that directs combustor exhaust gas onto the first-stage turbine rotor. This nickel-based superalloy component controls gas flow angle and throat area while managing extreme thermal conditions in the hot section. Installed within the high-pressure turbine stator assembly of gas-turbine engines, it requires dimensional inspection and cooling-passage verification before installation.
Mount and torque per engine manufacturer specifications and applicable maintenance 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 3075584-16 is a cooled high-pressure turbine nozzle segment that directs combustor exhaust gas onto the first-stage turbine rotor. This nickel-based superalloy component controls gas flow angle and throat area while managing extreme thermal conditions in the hot section.
Fuel system components are designed for specific fuel types per their engineering specifications. The NOZZLE SEGMENT, COOLED, HIGH PRESS should be verified against your aircraft's fuel system requirements. Currently available in: As Removed. Contact us for fuel compatibility details.
Many fuel system components require new gaskets, O-rings, or seals during installation. Check your aircraft maintenance manual for the NOZZLE SEGMENT, COOLED, HIGH PRESS installation requirements. We stock related sealing components and can help identify companion parts.
Most fuel system hardware ships via standard methods. Certain items containing fuel residue may require hazmat shipping procedures. We handle all packaging and shipping compliance. Same-day processing available for in-stock items.