DLA AN103101 THRU AN103200 REV 3-1986 BOLT - DRILLED HEX HEAD 1 HOLE 375-24.pdf

《DLA AN103101 THRU AN103200 REV 3-1986 BOLT - DRILLED HEX HEAD 1 HOLE 375-24.pdf》由会员分享，可在线阅读，更多相关《DLA AN103101 THRU AN103200 REV 3-1986 BOLT - DRILLED HEX HEAD 1 HOLE 375-24.pdf（1页珍藏版）》请在麦多课文档分享上搜索。

1、4.17 1s - I -,- IFED. SUP. CLASS. I L .625 .688 .750 .a12 .a75 .938 1 .o00 1 .o62 1.188 1.125 1.250 1.312 1.375 (a) -MATERIAL IDEtiTIFICATLON PEfi 2800. RAISED OR DEPRESSED . O10 MAX K TO FULL THD 016 OR CHAMFE .375-24UNF-3A SPEC MIL-S-7742 SECTION THRU THR 7 AN103106 I/ AN103107 1.562 AN103108 1.62

2、5 AN103109 1 688 AN103110 11:750 AN103114 2.000 AN103115 2.125 103116 2.250 Il AN103117 2.375 AN103118 II 2.500 _ K 1.000 - .o60 .430 ,562 ,625 .688 .750 .a12 .875 .938 1.000 1.125 1.250 1.375 1.500 _ .500 PART NO. 11 L 1 +.EO0 AN103120 2.750 1.750 - .o60 AN103119 2.625 1.625 103121 2.875 1.875 AN10

3、3122 3.000 2,000 AN103123 3.125 2.125 AN103124 3.250 2.250 AN103125 3.375 2.375 AN103126 3.500 2.500 AN103127 3.625 2.625 AN103128 3.750 2.750 AN103129 3.875 2.875 AN103130 4.000 3.000 AN103131 4 125 3.125 AN103132 I/ 4:250 I 3.250 THREAD TO HEAD. HAXIHUH TWO IHPERFECT THREADS. PART NO. AN103133 AN1

4、03134 AN103135 AN103136 AN103137 AN103138 AN103139 AN103140 AN103141 AN103142 AN103143 AN103144 AN103145 AN103146 K . L +.o00 - .o60 4.375 3.375 4.500 3.500 4.625 3.625 4.750 3.750 4.875 3.875 5.000 4.000 5.125 4.125 5.250 4.250 5.375 4.375 5.625 4.625 5.750 4.750 5.875 4.875 5.500 11.500 6.000 5.00

5、0 I PART NO. I AN103147 AN103148 AN103149 AN103150 - AN103151 AN103152 AN103155 2 AN103153 AN103154 I AN103156 AN103158 AN103157 4 I -THIS SURFACE MUST BE SQUARE WITH SHANK WITHIN .O03 FIR. LCHAMPER 30“ TO .562 DIA (OPPOSITE SIDE OPTIONAL) 103160 NB.TE: (1) SHANK SHALL BE STRAIGHT WITHIN .O025 FIR.

6、PER INCH OF BOLT LENGTH. (2) THE-CONCENTRTCLTY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN .O06 FIR. (3) THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER FACE DIAMETER AND HEXAGON SHALL BE WITHIN .O17 FIR. HATERIAL: STEEL ANS6322 HARDNESS: ROCKWELL C26-32 FINISH: CADHIHUH PLATE AMs

7、2400 SURFACE ROUGHNESS: ASID7 HANUFACTURING SPECIEICATIONS: AHS7452 INSPECTION: BREAK SHARP EDGES .O03 - .Dl5 UNLESS OTHERWISE SPECIFIED. ALL PARTS SHALL UNDERGO HAGNETIC INSPECTION IN ACCORDANCE WLTH AUS2640 DIHENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLERBNCES: LINEAR DIHENSIONS 2.010. ANGU

8、LAR DIHENSIONS 22. DO NOT USE UNASSTCNED PART NUHBERS. IS IP INACTIVE FOR NEW DESIGN AFTER 3 MARCH 1969 NO SUPERSEDING STANDARD. ;z THIS STANDARD WAS DEVELOPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILLTY PARTS COHHITTEE OF THE SAE. AIR FORCE-NAVY AERONAUTICAL STANDARD ANI03101 P.A. Air-Il THqU CUST . NAVY-A9 BOLT - DRILLED HEX HEAD, 1 HOLE, .375-24 . AN I O 3200 AR MY - AV Project No. 5306-1016 THIS DOCUMENT CONTAINS . PAGES. 1 I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-