1、 AN327493 THRU AN3277b REV 3 53 W 9977935 0000344 5 E 5s o/ I FED. SUP CLASS. I I Project No. 5307-0351 *U.S. GOVERNMENT PRINTING OFFICE 1986 - 805-038/43951 DOCUMENT CONTAINS -I- PAGES. I CHAMFER ,06245 Ans2800 .o10 UNDERSIZE AND OVERSIZE IDENTIFICATION STAMP PER S28 .O10 MAX DEPTH MX DEPTH INAC1 V
2、E FOR DESIGN AFTER 26 OCTOBER 1972. NO SUPERSEDING STANOARO NOTE: PITCH DIAMETERS OF BOTH THREADED ENDS SHALL BE CONCENTRIC WITHIN .O06 FIR. MATERTAL: STEEL AMS 6322. (AMs 6320 MATERIAL HAY ALSO BE USED FOR THESE PARTS UNTIL 1 JAN 1960.) HARDNESS: ROCKWELL C26-32. FINISH: -CADHIUM PLATE AMS 2400. DI
3、MENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN. SURFACE ROUGHNESS: AS 291 MANUFACTURING SPECIFICATION AMs 7456. BREAK SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIF1ED:TOLERANCES: LINEAR DIMENSIONS I.010. DO NOT USE INASSIGNED PART NUMBERS, THIS STANDA
4、RD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. 3 INSPECTION: ALL PARTS SHALL UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640. PA 11 AIR FORCE-NAVY AERONAUTICAL STANDARD AN 127493 THRU AN 127786 STUD - STRAIGHT, NECKED, -500-13 x .500-20 CUST AV, AS 11 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
