P/N: 6870811-p
Category: Circuit Breakers & Fuses
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 6870811-p is a front compressor diffuser for Rolls-Royce 250-C20B gas turbine engines. This high-temperature alloy component decelerates and directs compressor discharge air into the combustor section, conditioning airflow for efficient fuel mixing and combustion. Located downstream of the compressor stage, the diffuser reduces velocity while maintaining pressure recovery to optimize engine performance.
Installation and inspection follow Rolls-Royce M250 maintenance manual specifications and engine Illustrated Parts Catalog requirements. Critical for maintaining proper airflow dynamics in turbine engine operation.
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 6870811-p is a front compressor diffuser for Rolls-Royce 250-C20B gas turbine engines. This high-temperature alloy component decelerates and directs compressor discharge air into the combustor section, conditioning airflow for efficient fuel mixing and combustion.
Avionics compatibility depends on your aircraft model and existing installation. The FRONT COMPRESSOR DIFFUSER is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.