| Project Scope | Inner vane shroud repair |
| Capabilities Applied/Processes | Primary: Welding Brazing Conventional Machining EDM Machining Electron Beam Welding Secondary: Ultrasonic Cleaning Blending Deburring |
| Tightest Tolerances | ± 0.004" |
| Material Used | Nickel Alloy |
| Material Finish | As Cast, As Fabricated |
| Special Features | Replacement Ring is Fabricated, Machined, and Brazed into Place |
| In process testing/inspection performed | Fluorescent Penetrant Inspection |
| Industry for Use | Aerospace |
| Volume | 10 – 20 per Month |
| Delivery/Turnaround Time | 3 – 4 Weeks |
| Delivery Location | Customer Dock |
| Standards Met | Customer Specifications Federal Aviation Regulations Airworthiness Directives |
| Product Name | Pratt & Whitney JT/JFTD12 Turbine Engine First Stage Shroud |