DLA AN126767 THRU AN126820 REV 3-1986 STUD-STRAIGHT 5625-12 X 5625-18.pdf

《DLA AN126767 THRU AN126820 REV 3-1986 STUD-STRAIGHT 5625-12 X 5625-18.pdf》由会员分享，可在线阅读，更多相关《DLA AN126767 THRU AN126820 REV 3-1986 STUD-STRAIGHT 5625-12 X 5625-18.pdf（1页珍藏版）》请在麦多课文档分享上搜索。

1、AN12b767 THRU ANL26820 REV 3 53 m 9999935 0000447 4 MIN FULL THD CHAMFER .078x450 CHAMFER .O62x45O SECTION THRU APPROX THREAD PROFILE BOTH THD SIZES .5625-12HSJ -5625 -18UNF-3A UNDERSIZE AND OVERSIZE IDENTIFICATION STAMP SEE TABU FOR PD PER AM32800 ,010 MAX DEPTH IL-s-u UIYDERSIZE 9iNACTIVE FOR DES

2、GN AFTER 1 +.O03 AN126781 AN126787 OCTOBER IC +.O06 557 -.562 .5194 - .5204 .5199-.5214 .I 3 A +. O09 AN126783 AN126789 2. NO SUPERSEDING ST1 NOTE: PITCH DIAHETERS OF BOTH THREADED ENDS SHALL BE CONCENTRIC WITHIN ,006 FIR. ERIAL IATIFIGATIO1 IMP PER . DEPTH !a800 .o10 +.o12 ,566 -.571 .5254-.5264 .5

3、259-.5274 +?a LINEAR DIHENSIONS t.010. DO NOT USE UNASSIGNED PART NUHBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OP THE CAE. PA 11 AIR FORCE-NAVY AERONAUTICAL STANDARD AN 126767 THRU AN I26820 GUST: AV, AS STUD - STRAIGHT, -5625-12 x .5625-1& -1 11 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-