| Materials | Aerospace Grade Epoxy Adhesive Elevated Temperature Curing High Service Temperature Structural Paste Adhesive |
| Curing Method | Oven |
| Cure Rate | 1 Hour |
| Cure Temperature | >200° F |
| Surface Temperature - Retains Adhesive Properties To: | 450° F 100 psi / 6.9 MPa ASTM D1002 |
| Applications | Oil Pump |
| Adhesive Form | Thixotropic Paste |
| Pot Life | 8 hours (Room Temperature) |
| Adhesive Features | High Temperature Compatible with Aerospace Fluids Oil Resistant |
| Cleaning | Finish No. 4.1 Grit Blasting Finish No. 4.2. Hot Alkaline Cleaning Finish No. 4.3 Solvent Cleaning Blending Procedures (GE Standard Practices Manual 70-42-00) Light Duty Alkaline Cleaning (GE Standard Practices Manual 70-32-03) |
| Inspection | Coordinate Measuring Machine (CMM) Fluorescent Penetrant Inspection (FPI) SAE-AMS-STD-2175 Method 5.3.1 (Visual) Method 5.3.2.2 (Penetrant) ASQ-Z1.4 & ASQ – Z1.9 ISO-10012 & ANSI-Z540.3 Spot Fluorescent Penetrant Inspection (GE 70-32-03) |
| Testing | Certified Level II NDT Liquid Penetrant Non Destructive Testing (Mil-HNBK-728/1) |
| Quality Program | FAA 14 CFR Part 145 Compliance |
| Documentation | FAA Form 8130-3 (Airworthiness Approval Tag) |
| Additional Services | Repair Process Development Designated Engineering Representative (DER) |
| Production Volume | 1 to 30 parts |
| Typical Lead Time | 2 to 4 weeks |
| Industry Focus | Aerospace Military Commercial |
| Intended Applications | Turbine Components Oil Pump Components Fuel Pump Components Check Valve Assemblies |
| Air Agency Certification | FAA R91R0970 - Federal Aviation Administration EASA.145.5316 - European Aviation Safety Agency |
| File Formats | Modeling Capabilities |