1、 - _- I- - :ANI29605 THRU AN32990q REV 3 53 - 7999935 0000355 T - FED. SUP CLASS. I 5307 CHAMFER .047x450 SECTION THRU TiiREAD PROFILE BOTH TD SIZES STAm PEE AIS 2800 .OiOW DEPTH MIL-3-7742 UNDERSIZE AND OVERSIZE IDENTIFICATION STAMP DRILL N0.41 (.094-.101) PER AMs2800 .O10 MAX DEPTH CSK BO“% EMDS 6
2、00 TC .i50 DIA HOLE ON AXIS OF THREAD WITHIN .O05 UNDERSIZE - . O03 STANDARD ;.O03 +.O06 +.o09 +. 012 MD OVERSIZE tDEATIFICATIOA INACTIVE FOR DESIGN AFTER 26 OCTOBER 1972. NO SPERSEDING STANDARU I I Il I II I I I NOTE: PITCH DIAMETERS OF BOTH THREADED ENDS SHALL BE CONCENTRIC WITHIN ,006 FIR. HATERI
3、AL: STEEL AMS 6322. (AMs 6320 MATERIAL MAY ALSO BE USED FOR THESE PARTS UNTIL 1 JAN 1960.) HARDNESS: ROCKWELL C26-32. FINISH: CADMIUM PLATE AHS 2400. DIMENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN. SURFACE ROUGHNESS: AS 291 HANUFACTURING SPECIFICATION AMs 7456. BREAK SHARP EDGES .003-.O15 UNLESS OT
4、HERWISE SPECIFIED. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPEC1FIED:TOLERANCES; LINEAR DIMENSIONS I.OlO,ANGULAR DIMENSIONS I5O. DO NOT USE INASSIGNED PART NUMBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WLTH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. 3 INSPECTION: ALL PARTS SHAL
5、L UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640. I PA Il AIR FORCE-NAVY AERONAUTICAL STANDARD AN I29605 CUST-AV AS I THRU STUD - STRAIGHT, DRILLED, NECKED, .4375-14 x .4375-20 AN129904 Project No. 5307-0362 “a1.001Mm I- OIIICL lul.2l-lu*l J -. I THIS DOCUMENT CONTAINS / PAGES. *U.S. GOVERNMENT PRINTING OFFICE 1988 - 605-036/43909 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
