1、 , AN105001 THRU ANLOS100 REV 3 53 7737735 0000260 T H MATERIAL IDENTIFICATIJN PER 2800. RAISED OR DEPRESSED .O10 MAX 250 AN 1 O 5 O O 6 AN105007 1.000 1.062 1.125 PIJT NO, .188 AN105009 .250 105010 .312 105011 1.375 -562 1.438 .625 1 AN105015 AN105016 LTHIS SUAFACE MUST BE SQUARE WITH SHANK WITHIN
2、.O03 FULL INDICATOR RFADING CHAMFER 30 TO .625Du (OPPOSITE SIDE OPTIONAL) “i L K PART NO. +. O00 - .o60 - 1.500 .688 AN10501 1.562 .750 AN10501g 1.625 .812 AN105019 1.688 .875 105020 1. 50 .938 105021 2.000 1.188 10502 2.3-pi 1.562 AA105026 2.750 1.938 105029 1. LINEAR DIMENSIONS t.010, ANGULAR SHAN
3、K SHALL BE STRAIGHT WITHIN .O025 FIR.PER INCH OF BOLT LENGTH. THE JONCE?TICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIA .o06 FIR. THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHW FACE DUMETEn Am) HEIXAOOB CORROSION RESISTANT STEEL - SEE MANUPACTURING SPECIFICATION SHALL BE WITHIN
4、 -019 FR. Il DIKENSIONS f2 DO oT USE UNASSIGIiQ PART IilMSBS. rms STANDARD WAS DELOPED COOPERATILY WITX THE ENGINE AND PROPELLER UTILITY PARTS COMMIITBE OF TIE. SAE. NACTIVE FOR DESIGN AFTER 27 DEC 1966 NO SUPERSEDING STANDARD. AIR FORCE-NAVY AERONAUTICAL STANDARD AN i 5001 .A. tbrciist M - AV BOLT - CAES REX HEAD .4375-20 .AN; 8 % 100 w-u HW-IS Project No.5306-1034 / ! THIS DOCUblENT CONTAINS - 1 - PAGES. , Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
