1、 ANZ02001 THRU AN302Z00 REV 3 53 W 7977735 000023L 3 i- . FED. SUP CLASS. 5306 Il- CHAMFER .O31 x 45“ K TO FULL THD 7 APPROX- MATERIAL IDENTIFICATION PER AMS2800. RAISED OR DEPRESSED .O10 MAX .156 7z I 4 L.016 OR CHAMFER I ,491 MIN Ell .250-28UNF-3A SPEC MIL-S-7742 THIS SURFACE MUST BE SQUARE WITH
2、SHANK CHAMFER 30“ TO .438 DIA (OPPOSITE SIDE OPTIONAL) WITHIN .O03 FIR. SECTION THRU THREAD PROFILE II A 1.640 1.890 2.015 2.140 2.265 2.390 2.515 2.640 2.765 2.890 3.015 3.110 3.265 3.390 3.515 3.640 3.765 3.890 4.015 4:140 - 1.765 _- IC +.o00 -.o60 3.750 3.875 4,000 4.375 4.500 4.625 4 a756 4 .e75
3、 5.000 5.125 5.250 5.375 4.125 4.250 K k. O00 -. 060 - laal (a) (a) .188 .312 * 375 .438 .500 .125 .250 .562 .625 .688 .750 .812 - .875 .938 . O00 .o62 K + . O00 - .O60 1.125 1.250 1.375 1.500 1.625 1.750 1.875 2,000 2.125 2.2% 2 * 375 2.500 2.625 2.750 2.875 3.000 3.125 3.250 3.375 3.500 3.625 ;. P
4、ART NO. A 4.265 4 -390 4.515 4.640 :i$ 5.015 5.140 5.265 5.390 5.515 5 A40 PART NO. L 1.750 102006 1.875 102007 2. o00 102008 2.125 AN102010 2.375 AN102011 2.500 AN102012 2.625 AN102013 2.750 AN102009 2.250 102014 2.875 102016 3. i25 102018 3 I 775 102019 3.500 AN102015 3.000 AN102017 3.250 AN102020
5、 3.625 AN102021 3.750 AN102022 3.875 AN102029 4.750 AN102030 I/ 4 .875 AN102031 5 .O00 AN102050 AN102051 AH102052 AN10205 AN102055 AH102056 AH10205 Ml02052 M10d . .812 .702 .875 1 .765 ,938 .828 1.000 . .890 1.062 I .952 1.125 1.015 1.188 1.078 1.312 1.202 i 265 1.500 1.390 1.250 1.140 1:328 AN10204
6、0 AN102041 AN102042 AN102043 AN102044 AN102045 1.562 1.452 1,625 1.515 1.688 1.578 (a) THREAD TO HEAD. MAXIMUM TWO IMPERFECT THREI SHANK SHALL BE STRAIGHT WITHIN .O03 FIR.PER INCH OF BOLT LENOTH. THE CONCENTRICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN .o06 FIR THE CONCENTXICITY OF TH
7、E SHANK IN RELATION TO THE WASHER FACE DIAIBTBI AND HEXMOW SHALL BE WITHIN .O13 FIR. MATERIAL: STEEL AMs6322 HARDNESS: ROCKWELL C26-32 FINISH: CADMIUM PLATE AMS2400 SURFACE ROUGHNESS: AS107 MA“ACTLTR1NG SPECIFICATION: AMS7452 INSPECTION ALL PARTS SHALL UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH
8、2640 BREAK SHARP EWES .003-.015 UNLESS OTHERWISE SPECIFIED. DIIIENSIOHS IN INCHES. DO NOT USE UNASSIGNED PART FERS. U(iLE3.S OTHERWISE SPECIFIED: TOLERANCES; LINEAR DIMENSIONS f.010, AWOULAR DIMENSIONS f2 . INACTIVE FOR NEW DESIGN AFTER 3 MARCH 1969 NO SUPERSEDING STANDARD.- AN 102001 THIS STANDARD WAS DEVELOPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILITY PARTS COI+IITTEE OF SM. AIR FORCE-NAVY AERONAUTICAL STANDARD P.A. Af-II THRU Project tio. 6306-1005 I - I . .- . . - Licensed by Information Handling Services
