| Project Scope | Salvage repair of the discharge nozzle combustion liner assembly |
| Capabilities Applied/Processes | Primary: Welding Blending Brazing Secondary: Abrasive Blasting |
| Overall Part Dimensions | Length: 5.125" Width: 6.500" |
| Tightest Tolerances | ± 0.0035" |
| Material Used | Frame: C242 Nickel Alloy, Body: C263 Nickel Alloy
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| Material Finish | As Formed, No Coating |
| In process testing/inspection performed | Fluorescent Penetrant Inspection |
| Industry for Use | Aerospace |
| Volume | 500 per Year |
| Delivery/Turnaround Time | 2 – 3 Weeks |
| Delivery Location | Customer Dock |
| Standards Met | Customer Specifications, Rolls-Royce Standards |
| Product Name | Discharge Nozzle Combustion Liner Assembly |