| AIRCRAFT LOCATION | LEADING EDGE FLAP |
| AIRCRAFT MISSION DESIGN SERIES | F35 |
| FURNISHED ITEMS | NUT PLATE |
| HEIGHT | 3.480 INCHES NOMINAL |
| HOLE QUANTITY | 8 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4050 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.090 INCHES MINIMUM AND 0.126 INCHES MAXIMUM |
| III MATERIAL | ALUMINUM ALLOY 7050 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT ASSEMBLY, INTERIM NO 2-LEADING EDGE FLAP |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 5.280 INCHES MINIMUM AND 5.530 INCHES MAXIMUM |
| OVERALL WIDTH | 2.450 INCHES NOMINAL |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 TYPE 1B MIL SPEC SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | ANODIZE |