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| Session 1 | ||||
| Location: Mercer A & B (Hilton Seattle Airport & Conference Center) | ||||
| (Please check final room assignments on-site). | ||||
| Session Description: | ||||
| Session Chair: | Dr. Eun Lee NAVAIR-Naval Air Systems Command, Patuxent River, MD | |||
| 1:30 PM | EIF1.1 | F-14 Arresting Gear Stingers - Failure Analysis, Prevention, and Significant Technical Aspects | ||
| 2:00 PM | EIF1.2 | Failure Analysis of an Aircraft NLG Cam Follower End Washer | ||
| 2:30 PM | EIF1.3 | F-15 Wing Pylon Rib Corrosion Fatigue Detection & Inspection/Repair | ||
| 3:00 PM | Break | |||
| 3:30 PM | EIF1.4 | Application of the Spiral Notch Torsion Test Method to Stress-Corrosion Cracking | ||
| 4:00 PM | EIF1.5 | Fractographic Analysis of Cracks from a Full-Scale Fatigue Test | ||
| 4:30 PM | EIF1.6 | Failure Analysis of Turbine Engine In-Flight Failure | ||
| 5:00 PM | EIF1.7 | The Effect of the Forging Process on Component Fatigue | ||