| MATERIAL | ALUMINUM ALLOY OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4135 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CONNECTION TYPE | THREADED EXTERNAL TUBE 1ST END |
| FLANGE 2ND END |
| CONNECTION STYLE | INVERTED FLARE (TUBE) 1ST END |
| SEAT ANGLE | 37.0 DEGREES 1ST END |
| FLANGE SHAPE | TRIANGULAR WITH HOLES 2ND END |
| NOMINAL THICKNESS | 0.310 INCHES 2ND END |
| BOLT HOLE QUANTITY | 3 2ND END |
| BOLT HOLE NOMINAL DIAMETER | 0.286 INCHES 2ND END |
| BOLT CIRCLE NOMINAL DIAMETER | 1.602 INCHES 2ND END |
| FLANGE FACE DESIGN | RAISED WITH CURVE AND COUNTERBORE 2ND END |
| RAISED FACE NOMINAL HEIGHT | 0.369 INCHES 2ND END |
| RAISED FACE NOMINAL DIAMETER | 0.909 INCHES 2ND END |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.750 INCHES 1ST END |
| THREAD SERIES DESIGNATOR | UN 1ST END |
| NOMINAL THREAD SIZE | 1.188 INCHES 1ST END |
| THREAD QUANTITY PER INCH | 12 1ST END |
| THREAD CLASS | 2A 1ST END |
| LEG LENGTH | 2.499 INCHES NOMINAL 2ND END |
| FLOW ANGLE | 90.0 DEGREES |
| SPECIAL FEATURES | A FAILURE COULD CAUSE CATASTROPHIC OR CRITICAL FAILURE RESULTING IN THE LOSS OF OR SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM |