1、I AN129233 THRU AN129292 REV 3 53 W 7999935 0000353 b W I AIR FORCE-NAVY AERONAUTICAL STANDARD PA 11 CUST AV, AS i STUD - STRAIGHT, DRILLED, .625-11 x .625-18 i1 i - AN I29233 THRU AN129292 FE%. SUP CLASS. 5307 o (a) MAX PULI. OR IMPERFECT THD- +2 THD (a) MAX FULL OR IMPERFECT THD- ,d A+2 THD MIN F
2、OLL THD CHAMFER ,06245 APPROX MIN FULL THD CYAMFER .07845 APPROX - SECTION THRU THREAD PROFILE BOTH THD SIZES LiuTL IDXNT .CO-.AJJr -11NS FOR PD OP RIREAD WITHIN ,005 .625-18UNF-3A MIL-S-7742 STAl PER AMs2800 .O10 IUX DeFm UNDERSIZE AND OVERSIZE- SEE TABL IDENTIFICATION STAMP PER AM52800 .O10 MAX DE
3、PTH +.o12 529 -.634 i832 - .5842 ,837-.5852 ,760-.578C ART NUMBEF AN129250 AN129256 AN129262 TANDARI t. o09 STANDARD t.006 I UHDERSIZE AND - .O03 OVERSIZE DENTIFICATION 529 -.634 j802-.5812 j807-.5822 j730-.5750 ART NUMBER 520 -.625 j772-.5782 5777-.5792 ZT NUMBER 700-.5720 620 -.625 5712-.5722 5717
4、5732 640-. 5660 :E“ NUMBER 620 -.625 5682 - .5692 5687-.5702 5610- .5630 ART NUMBER D BE D AF L e - ? .375 ?.438 2.750 I 3E PLATING i PLATING - B - L.OOC 1.ooc 1. ooc IVE THRE A - L.250 1.312 L.562 IAC AN129248 AA129254 AN129260 AN129249 AN129255 129261 AN129247 AN129253 AN3.29259 AN129246 A111129
5、252 AN129258 :OR DES iN AFTER 26 OCTOBER 1972. NO SUPERSEDING Il I II I I I NOTE: (a) HATERIAL: STEEL AMS 6322 HARDNESS: ROCKUELL C26-32. FINISH: PITCH DIAMETERS OF BOTH TBREADED ENDS SHALL BE CONCENTRIC WITHIN .O06 FIR. CROSS THREADING PERMISSABLE AT THREAD RUNOUTS ON SHORT STUDS. (AMS 6320 MATERIA
6、L HAY ALSO BE USED FOR THESE PARTS UNTIL 1 JAN 1960) CADHIUH PLATE AHS 2400. DIMENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN. Il I I Project No. 5307-0360 THIS DOCUMENT CONTAINS -I - PAGES. 1 *U.S. GOVERNMENT PRINTING OFFICE: 1986 - 605-036/43908 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
