DLA AN101301 THRU AN101400 REV 3-1986 BOLT - HEX HEAD 375-24.pdf

《DLA AN101301 THRU AN101400 REV 3-1986 BOLT - HEX HEAD 375-24.pdf》由会员分享，可在线阅读，更多相关《DLA AN101301 THRU AN101400 REV 3-1986 BOLT - HEX HEAD 375-24.pdf（1页珍藏版）》请在麦多课文档分享上搜索。

1、- ANLOL303 THRU AN301400 REV 3 53 W 7797935 0000225 8 W .t I L -750 .a12 .a75 .938 1.000 1.062 1.125 1. lea 1.250 1.312 1.438 1.375 MATERIAL IDENTIFICATION PER AMS2800. RAISED OR DEPRESSED .o10 MAX I SECTION THRU THREAD PR( K +.O00 PART NO. L - .o60 1.500 1.562 (a) 101306 1.625 (a) AN101307 1.688 .1

2、25 AN101308 1.750 .i88 AN101309 1.875 .250 101310 2.000 .312 101311 2.125 .375 AN101312 2.250 .438 AN101313 2.375 .500 AN101314 2.500 .562 AN101315 2.625 .625 AN101316 2.750 .688 AN101317- 2.875 PED. SUP. CLASS. K TO FULL THD SPEC MIL-S-7742 rLe K + . O00 -.o60 -750 .a12 .e75 -938 1.000 1.125 1.250

3、1.375 1.500 1.625 1.750 1.875 2.000 2.125 THIS SURFACE MUST BE SQUARE WITH SHANK WITHIN .O03 FIR. CHAMFER 30 TO .562 DIA (OPPOSITE SIDE OPTIONAL) PART NO. L . AN101318 3 .O00 AN101319 3.125 AN101320 3.250 101321 3.375 101323 3.625 AN101322 3.500 AN101324 3.750 AN101325 3.875 101326 4 .O00 AN101327 4

4、.125 AN101328 4.250 AN101329 4.375 AN101330 4.500 AN101331 4.625 K + . O00 - .o60 2.250 2.375 2.500 2.625 2.750 2 :a75 -3.000 3.125 3.250 3 * 375 3.500 3.625 3 e750 3.875 II I l K - .o60 PART NO. L +.O00 PART NO. AN101332 4.750 4.000 AN101346 AN10133 4 875 4.125 AN101347 AN101332 11 51000 1 4.250 1

5、ANlOl3M AN101335 5.125 4.375 AN101349 5.250 4.500 AN101350 %Et:; I( 5.375 i 4.625 1 AN101351 AN101338 5 .SOO 4.750 AN101352 AN101339 5.625 4.875 AN101353 AN101340 5.750 5 .O00 AN101354 AN101341 5.875 5.125 AN101355 AN101342 6.000 5.250 AN101356 AN101343 (a) THREAD TO HEAD. MAXIMUM TWO IMPERFECT THRE

6、ADS SHANK SHALL BE STRAIGHT WITHIN .O025 FIR.PER INCH OF BOLT LENGTH. THE CONCENTRICIPY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN .O06 FIR. THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER FACE DIAMETER AND HXAGON .-. SHALL BE WITHIN .O17 FIR. MATERIAL: STEEL AMs6322 HARDNESS: RO

7、CKWELL C26-32 FINISH: CADMIUM PLATE AMs2400 SURFACE ROUGHNESS: AS107 MANWACTIIRING SPECIFICATION: AMS7452 INSPECTION: ALL PARTS SHALL UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640. BREAK SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED, DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLE

8、RANCES; LINEAR DIMENSIONS f.O1O, ANGULAR DIMENSIONS f2 O. DO NOT USE UNASSIGNED PART NUMBERS. INACTIVE FOR NEW DESIGN AFTER 3 wm 1969 NO SUPERSEDING STANDARD. THIS STANDARD WAS DEVELOPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. AIR FORCE-NAVY AERONAUTICAL STANDARD I AN I 0 I 30 P.A. AF-II IYPII Y o a r E - C c r . L P c r 5 2 4 U -I 4 I P i r Iu c 3 O 3 e C - 1.1“ CUST. NAVY- AC BOLT - HEX HEAD .375-24 5306-0998 THIS DOCUMENT CONTAINS 1 PAGES. - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-