1、i ANL30177 THRU AN130478 REV 3 53 7777715 0000357 3 M PA 11 IR FORCE-NAVY AERONAUTICAL STANDARD STUD - STRAIGHT, DRILLED, NECKED, .5625-12 x .5625-18 a AN I30 I99 THRU AN I30498 FED. Sfi CLASS. 5307 HAMFER .062x45 CHAMFER ,07845 APPROX STAW PEE AUS 2800 SECTION THRU THREAD PROFILE BOTH THD SIZES UND
2、ERSIZE AND OVERSIZE IDENTIFICATION STAMP PER AM92800 .O10 MAX DEPTH .o10 WX DEPTH UNDERSIZE AND OVERSIZE IDENTIFICATION C PD BEFORE PLATINO PD AFTER PLATINO .5625-12NS SEE TABLE FOR PD 60 TO .188 DIA HOLE ON AXIS OF THREAD WITHIN .O05 I -.O03 I STANDARD 1 INACTIVE FOR DESIGN -AFTER LINEAR DIMENSIONS
3、 I.OIO,ANGULAR DIMENSIONS f5. DO NOT USE INASSIGNED PART NUMBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE CAE. 9 INSPECTION: ALL PARTS SHALL UNDERGO MAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640. *U.S GOVERNMENT PRINTING OFFICE 1986 - 605-OW43911 THIS DOCUMENT CONTAINS 1- - PAGES. ) - - Licensed by Information Handling ServicesProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
