1、 AN105101 THRU AN105200 REV 3 53 7777715 0000261 1 r I FED. SYS6CLASS MATERIAL IDENTIFICATION PER AIIS2800. RAISED OR DEPRESSED .o10 MAX .2 81 K TO FULL THD- CHAMPEE *O47 x 45” APPOX .O16 OR CHAMFER - d SE8TION THRU THREAD PROFILE - -500-20 W-3A SPEC MIL-S-7742 -THIS SURFACE MUST BE SQUARE WITH SHAN
2、K WITHIN .O03 FULL INDICATCR READING CHAMFER 30 T0.750 DIA (OPPOSITE SIDE OPTIONAL) 1.500 .60 AN105115 3.000 2.125 nnio512g 4. 50 1.562 .688 AN105116 3.125 2.250 nrriogi30. 4.;: (a) THREAD TO HEAD. HAXIHUH TWO IHPERFECT THREADS. PART NO. AN105131 AN105133 AN105134 AN105135 AM05136 AN105137 AN105138
3、AN105139 AN105140 AN105141 AN105142 AN105143 AN105144 105132 L - 5.000 5.125 5.250 5.575 5.625 5.750 5.875 6.000 5.500 +.o00 - .o60 4.125 ATJ105l.4: 4.250 AN105146 4.375 AN105147 4.500 AN10514E 4.625 AN105145 4.750 AN105150 NOTE: (1) SHANK SHALL BE STRAIGHT WITHIN .O02 FIR. PER INCH OF BOLT LENGTH.
4、2) (3) THE CONCENTRICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER FACE DIAHETER AND HEXAGON .O06 FIR. SHALL BE WITHIN .O23 FIR. INACTIVE FOR DESIGN AFTER 27 DEC 1966 NO SUPERSEDING STANDARD. HATERIAL: SURFACE ROUGHNESS: AS107 HAN
5、UFACTURIHG SPECIFICATION: AUS 7472 BREAK SHARP EDGES DIHENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: DO NOT USE UNASSIGNED PART NUHBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COHHITTEE OP THE CAE. CORROSION RESISTANT STEEL - SEE HANUFACTURING SPECIFI
6、CATION ) INSPECTION: ALL PARTS SHALL UNDERGO FLUORESCENT PENETRANT INSPECTION IN ACCORDANCE WITH AHS2645. .003-.015 UNLESS OTHERWISE SPECIFIED. TOLERANCES; LINEAR DIHENSIONS 2.010. ANGULAR DIMENSIONS t2. P.A. AIR FORCE-NAW AERONAUTICAL STANDARD USAI - II Navy - AS Army - AV Other Cust BOLT - CRES HEX HEAD .500-20 I I J .y1 WM.*T?8nZOEL ,*,a,. “I.,. Project No. 5306-1035 THIS DOCUMENT CONTAINS -1 PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
