| FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 0.562 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
| FIRST LEG LENGTH | 0.750 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| FIRST LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| FIRST LEG HOLE DIAMETER | 0.097 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| FIRST LEG STYLE | CORNER RADIUS |
| FIRST LEG THICKNESS | 0.040 INCHES NOMINAL |
| FIRST LEG WIDTH | 1.125 INCHES NOMINAL |
| FSC APPLICATION DATA | SPAR ASSEMBLY,CENTER SECTION FRONT,AIRCRAFT |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 0.500 INCHES NOMINAL |
| SECOND LEG LENGTH | 1.125 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | END RADIUS AND TAPERED |
| SECOND LEG END RADIUS | 0.250 INCHES NOMINAL |
| SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| SECOND LEG HOLE DIAMETER | 0.097 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| SECOND LEG THICKNESS | 0.040 INCHES NOMINAL |
| SECOND LEG WIDTH | 1.125 INCHES NOMINAL |
| STYLE DESIGNATOR | ANGLE |
| SURFACE TREATMENT | CHROMATE |