| CRITICALITY CODE JUSTIFICATION | FEAT |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.310 INCHES NOMINAL |
| FIRST LEG END RADIUS | 0.500 INCHES NOMINAL |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG HOLE DIAMETER | 0.219 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.310 INCHES NOMINAL |
| FIRST LEG STYLE | END RADIUS |
| FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
| FIRST LEG WIDTH | 0.625 INCHES NOMINAL |
| FIRST LEG LENGTH | 0.680 INCHES NOMINAL |
| FSC APPLICATION DATA | ENGINE,ACFT,TURBO-FAN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6350 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL | STEEL COMP 4130 |
| SECOND LEG END RADIUS | 0.500 INCHES NOMINAL |
| SECOND LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| SECOND LEG HOLE DIAMETER | 0.281 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.310 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.310 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
| SECOND LEG WIDTH | 0.625 INCHES NOMINAL |
| SECOND LEG LENGTH | 1.060 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | END RADIUS |
| SPECIAL FEATURES | FAILURE COULD CAUSE CATASTROPHIC OR CRITICAL FAILURE RESULTING IN THE LOSS OF OR SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM OR AN UNCOMMANDED ENGINE SHUTDOWN THAT JEOPARDIZES SAFETY |
| STYLE DESIGNATOR | ANGLE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS 2400 ASSN STD SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | CADMIUM |