| AIRCRAFT LOCATION | STRUCTURAL COMPONMENT |
| AIRCRAFT MISSION DESIGN SERIES | F/A-18 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | 7075 AL ALY, COND T7351 PER MMS 159 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.250 INCHES NOMINAL |
| III MATERIAL | ALUMINUM ALLOY 7075 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER STRAP - LWR CAP,SPAR ?,STRESS CORROSION CRACKING |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 7.940 INCHES NOMINAL |
| OVERALL WIDTH | 0.680 INCHES NOMINAL |
| SPECIAL FEATURES | NHA: 74A092304 |