DLA AN101601 THRU AN101700 REV 3-1986 BOLT - HEX HEAD 5625-18.pdf

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1、 _ !AN303601 THRU AN303700 REV 3 53 M 7777735 0000228 3 = 3- 17-q L - 1.062 1.125 1.188 1.250 1.312 1.375 1.438 1.500 1.562 1.625 1.688 - S - K + . O00 - .O60 .125 .188 .250 .312 .375 .438 .500 .562 .625 .688 .750 I I TION THRU THREAD PROFILE -lr- AN101606 11 2.000 AN101607 2.125 AN101608 2.250 AN10

2、1609 2.375 AN101610 11 2.503 101611 2.625 AN101615 3.125 AN101616 I/ 3.250 K + . O00 - .O60 .a12 .a75 .938 1.062 1.188 1.312 1.438 1.562 1.688 1.812 1.938 2.062 2.188 2.312 LTHIS SURFACE MUST BE SQUARE WITH SHANK WITHIN .O03 FIR. LCHAMFER 30“ TO .875 DIA (OPPOSITE SIDE OPTIONAL) AN101617 3.375 AN101

3、618 (I 3.500 AN101619 3.625 AN101620 3.750 AN101622 4.000 II 101621 3 .a75 AN101623 4.125 AN101624 4.250 AN101625 4.375 101626 4.500 AN101627 4.625 AN101628 4.750 K + . O00 - .O60 2.438 2.562 2.688 2.812 2.938 3.062 3.188 3.438 3.562 3.688 3.938 3.312 3.812 4 .o62 PART NO. II L AN101631 5.125 AN1016

4、32 11 5.250 AN101633 5 a375 AN101634 5.500 AN101635 11 5.625 AN101636 5.750 AN101637- 5.875 AN101638 11 6.000 AN101639 AN 1 O1 64 3 AN101644 /I II K t. . O00 - .O60 4.188 4.312 4.438 4.562 4.688 4 .a12 4.938 5.062 PART NO. AN101645 AN101647 101646 AN101648 AN101649 AN101650 AN101651 AN101652 NOTE: S

5、HANK SHALL BE STRAIGHT WITHIN .O02 PIR.PER INCH OF BOLT LENGTH. THE CONCENTRICITY OF THREAD PD IN-RELATION TO THE SHANK SHALL BE WITHIN THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER FACE DIANETER AND HEXAGON .O06 FIR. (3) SHALL BE WITHIN .O26 FIR. MATERIAL: STEEL AMs6322 HARDNFSS: ROCKhEL

6、L C26-32 FINISH: CADMIUM PLATE AMs2400 SURPACE ROUGHNESS: AS107 MANUFACTURING SPECIFICATION: AMs7452 0 INSPECTION: ALL PARTS SHALL UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640. BREAK SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED. DIMENSIONS IN INCHES. UNLESS OTWWISE SPECIFIED: TOLERANCE

7、S; LINEAR DIMENSIONS f.010, ANGULAR DIMENSIONS t2 O. DO NOT USE UNASSIGNED PART NUMBERS. INACTIVE FOR NEW DESIGN AFTER 3 “1969 NO SUPERSEiNG STANDARD. THIS STANDARD WAS DEVELOPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. I AIR FORCE-NAVY AERONAUTICAL STANDARD I ANI01 601 P.A. AF-Il I THRU BOLT - HU HF.K rr- -“ CUSf. NAVY- AS ARMY-AV THIS DOCUMENT CONTAINS / iHbt* - _& .-. I- 5306-io01 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-