1、875 AN149099 4.250 .3,000 AN149100 4.500 3.250 AN149102 4.625 3.375 AN14910 4.750 3.500 AN149102 3.375 2.125 AN149093 4.375 3.125 - AN149101 - 1.312 1.375 1.438 1.500 1.625 1.562 3i tA .18 .250 .312 -375 v 6.000 - SECTION THRU THREAD PROFILE 4.750 AN149114 4- - .o60 ?A Il AIR FORCE-NAVY AERONAUTICA
2、L STANDARD CUST AV, AS I BOLT - SOCKET HEAD, 6 HOLES DRILLED, .SoOs20 I 11 AN149051 AN149150 THRU PART NO. AN149064 AN149065 AN149066 AN 1 49 067 AN 149 068 AN149069 AN149070 AN149071 AN149072 AN 14907 3 AN 1 49 07 4 AN149075 AN149076 .245 MATERIAL IDENTI- FICATION .O10 MAX DEPRESSION .150 .WO THIS
3、SURFACE MUST BE SQUARE WITH SHANK WITHIN .O03 FULL INDICATOR READIN 4.000 AN149108 55:;:; I 4.125 1 AN149109 5.500 4.250 AN149110 5.625 4.375 AN149111 AN1491 12 5.750 1 :V& 1 5.875 AN149113 (a) THREAD TO HEAD. MAXIHUM TWO IMPERFECT THREADS. NOTE: (I) THE RUNOUT FOR STRAIGHTNESS OF SHANK SHALL NOT EX
4、CEED .O02 FIR PER INCH OF BOLT LENGTH. (2) THE CONCENTRICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN a006 FIR. (3) THE CONCENTRICITY OF THE HEXAGON SOCKET IN RELATION TO OD OF HEAD SHALL BE WITHIN -005 FIR, (4) THE CONCENTRICITY OF THE SHANK IN RELATION TO OD OF HEAD SHALL BE WITHIN ,0
5、05 FIR. HATERIAL: STEEL AHS 6322 HARDNESS: ROCKWELL C32-36 FINISH: CADMIUH PLATE ANS2400 SURFACE ROUGHNESS: AS107 MANUFACTURING SPECIFICATION: AMS7452 INSPECTION: ALL PARTS SHALL ULDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640. BREAK SHARP EDGES .003-.O15 UNLESS OTHERWISE SPECIFIED. !NACTIVE
6、FOR DESIGN AFTER I JAN 1960 SEE DRAWING MS9093 For definition and application of drawing status notes. see ANA Bulletin No. 337. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE I Project No. 5306-1071 I THIS DOCUMENT CONTAINS -11 PAGES. 1 *U.S. GOVERNMENT PRINTING OFFICE 1966 - 605-036143939 ,-, I - ,?L - - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
