1、PED. SUP. CLASS. 5306 -0 n MATERIAL IDENTIFICATION PER AMS2800. RAISED OR DEPRESSED .O10 MAX - _i y- 562 2.688 .2.812 2.938 3.062 3.188 3.312 3.438 3.562 3.688 3.812 AN101437 5.500 AN101438 5.625 AN101439 5.750 AN101440 5.875 101441 6.000 AN101442 AN101443 II AN101444 K + . O00 - .O60 3.938 4.062 4.
2、188 4.312 4.438 4.562 4.688 4.812 4.938 5.062 5.188 PART NO. AN1014a5 AN101446 AN101447 AN101448 AN101449 AN101450 AN101451 AN101452 AN101453 AN101454 AN101455 (a) THREAD TO HEAD. MAXIMUM TWO IMPERFECT TH?.EADS. SHANK SHALL BE STRAIGHT WITHIN .O025 FIR.PER INCH OF BOLT LENGTH. THE CONCENTRICITY OF T
3、HREAD PD IN RELATION TO THE SHANK SHALL BE-WITHIN .O06 FIR. THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER FACE DIAMETER AND HEXAGON SHALL BE WITHIN .O19 FIR. I MATERIAL: STEEL Am6322 HARDNESS: ROCIWELL C26-32 FINISH: CADMIUM PLATE Abt32400 SWACE ROUGHNESS: AS107 MANUFACTURING SPECIFICATIO
4、N: Am7452 3 INSPECTION: ALL PARTS SHALL UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH -640. FlREXK SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLERANCES; LINEAR DNSIONS 1.010, ANGULAR DIMENSIONS f2“. DO dT USE UNASSIGNED PART NUMBERS. INACTIV
5、E FOR NEW DESIGN AFTER 3 JXR 1969 NO SUPERSEDING STANDARD. THIS STANDARD WAS DEVELOPED COOPERATIVELY B“ THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. AIR FORCE-NAVY AERONAUTICAL STANDARD ANI 01401 AN I O I500 P.A. AF-II niau CUST. NAVY- AS BOLT - HEX HEAD -4375-20 ARMY -AV / I 7 5306-0999 THIS DOCUMENT CONTAINS / PAGES. Licensed by Information Handling ServicesProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
