| BODY THICKNESS | 0.050 INCHES NOMINAL |
| CORNER BEVEL LENGTH | 0.120 INCHES NOMINAL |
| CROSS-SECTIONAL SHAPE STYLE | FLAT |
| DISTANCE BETWEEN HOLES ALONG WIDTH | 2.860 INCHES NOMINAL |
| DISTANCE BETWEEN HOLES ALONG LENGTH | 1.875 INCHES NOMINAL |
| FSC APPLICATION DATA | GROUND SUPPORT EQUIPMENT F-18 AIRCRAFT |
| HOLE QUANTITY ALONG WIDTH | 4 |
| HOLE QUANTITY ALONG LENGTH | 2 |
| LENGTH | 6.410 INCHES NOMINAL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AQQ-A-250/11 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL | ALUMINUM ALLOY 6061 |
| PERIPHERAL SHAPE STYLE | RECTANGLE, MULTI HOLES |
| SECURING DEVICE TYPE | HINGE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-83286 MIL SPEC SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | ENAMEL |
| WIDTH | 6.060 INCHES NOMINAL |