| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 TYPE 1B MIL SPEC SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | ANODIZE |
| AIRCRAFT LOCATION | LEADING EDGE FLAP |
| AIRCRAFT MISSION DESIGN SERIES | F35 |
| FURNISHED ITEMS | NUT PLATE |
| HEIGHT | 3.380 INCHES NOMINAL |
| HOLE QUANTITY | 8 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4050 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.150 INCHES MINIMUM AND 0.155 INCHES MAXIMUM |
| III MATERIAL | ALUMINUM ALLOY 7050 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT ASSEMBLY, INT, LEADING EDGE FLAP, LH |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 4.68 INCHES NOMINAL |
| OVERALL WIDTH | 2.45 INCHES NOMINAL |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| SPECIAL FEATURES | NEXT HIGHER ASSEMBLY OF BULLNOSE INSTALLATION-LEFT; 8 HOLES |