1、AN103001 THRU AN103100 REV 5 CANC 9 9999915 0002951 911 E L ,500 .562 .625 .688 e750 .812 .o15 ,938 1.ooO 1.062 1.125 1.188 1.250 (8) T FSC 5306 s- K TO PULL THD DRILL NO. 50 CSINK 90. To /s w L 1 II Y -:3IA .3125-24UHP-3A /V-lk i SPEC MIL-S-7742 THIS SURFACE MUST BE SOUAR- WITH SHANK WITHIN .O03 FI
2、R. K -.o00 -.: AN103041 5.250 4.375 AN103042 5.375 4.500 AN103043 5.500 4.625 AN103045 5.750 4.815 AN103045 5.875 5.000 AN103044 5.625 4.750 , 6.000 , 5.125 PART NO. AN103049 AN103050 AN103052 AN103051 AN10305 AN103052 AN103055 AN103056 AN103057 AN103058 AN103059 103060 AN109061 SHANK SHALL BE SEAIG
3、HT WITHIN .o03 FIR.PER INCH OF BOLT LENGTH. THE CONCENTRICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN .O06 FIR. THE CONCENTRICITY OP THE SHANK IN RELATION TO THE WASIW FACE DIAKETER AND HEXAGON 3) SHALL BE WITHIN .O15 FIR. MATERIAL: STEEL 6322 HARDNESS: ROCKWELL C26-32 FINISH: CADMIUM
4、PLATE AMS2430 SURFACE ROUGHNESS: AS107 MANUFACTURING SPECIFICATION: AM.57452 PARTS SUBJECT TO MAGNETIC INSPECTION PER m26110. BREAK SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED. DIKENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLERANCES; LINEAR DImSIONS 2.010, ANGULAR DIWENSIONS 22. DO NOT USE
5、 UNASSIGNED PART HUEIBERS. 8 CANCELED AS OF 9 OCT 87 INACTIVE FOR NEW DESIGN AFTER 3 MAR: LW No SUPERSEMNG STANDARD. THIS STANDAN) WAS DkTMPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OP THE SAE. - E:E;g TR FORCE-NAVY AERONAUTICAL STANDARD I AN103001 i- I THRU I AN103100 BOIT - DP.IU3 HSX HEAD, 1 HOLE. .3125-24 um mtm omcr; LI.YI.IIVLI) - i L.- LIII Project 5306- 1YOF Licensed by Information Handling Services
