| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.650 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.340 INCHES NOMINAL |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG LENGTH | 1.530 INCHES NOMINAL |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG HOLE DIAMETER | 0.204 INCHES MINIMUM AND 0.212 INCHES MAXIMUM |
| FIRST LEG WIDTH | 0.720 INCHES NOMINAL |
| FIRST LEG STYLE | SQUARE AND TAPERED |
| FIRST LEG THICKNESS | 0.094 INCHES NOMINAL |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 T851 FED SPEC 1ST MATERIAL RESPONSE OR QQ-A-200/3 T8511 FED SPEC 2ND MATERIAL RESPONSE |
| MATERIAL | ALUMINUM |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET ASSERMBLY |
| PROPRIETARY CHARACTERISTICS | PACS |
| MOUNTING HOLE TYPE | PLAIN |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.320 INCHES NOMINAL |
| SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 0.560 NOMINAL INCHES |
| SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| SECOND LEG HOLE DIAMETER | 0.098 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.370 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | SQUARE AND TAPERED |
| SECOND LEG THICKNESS | 0.094 INCHES NOMINAL |
| SECOND LEG WIDTH | 0.720 INCHES NOMINAL |
| SECOND LEG LENGTH | 1.750 INCHES NOMINAL |
| SPECIAL FEATURES | NAME CHANGED FROM BRACKET, STRUCTURAL OMPONENT, AIRCRAFT |
| STYLE DESIGNATOR | ANGLE |