1、_- . AN230977 THRU AN130774 REV 3 53 7777735 O000358 5 m HAMFER .062x45 CHAMFER .078x45 ID ENT IFICATIO STAMP PER DRILL NO. 30 (.115-.133) CSK BOTH ENDS AMC2800 .O10 60 TO .I88 DIA MAX DEPTH HOLE ON AXIS OF THREAD WITHIN .O05 .625-18UNF-3A MIL-S-7742 SECTION THRU THREAD PROFILE UNDERSIZE AND OVERSIZ
2、E IDENTIFICATION STAMP PER AMS2800 .O10 MAX DEPTH SEE TABLE FOR PD OVERSIZE IDENTIFICATION NOTE: MATERIAL: STEEL AMS 6322. HARDNESS: ROCKUELL C26-32. FINISH: CADMIUM PLATE AMS 2400. DIMENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN. SURFACE ROUGHNESS: AS 291 MANUFACTURING SPECIFICATION ANS 7456. BREAK
3、 SHARP EDGES .003-.015 UNLESS OTHERWISE SPECIFIED. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPEC1FIED:TOLERANCES: LINEAR DINENSIONS +.DlO,ANCULAR DIMENSIONS +5O. DO NOT USE INASSIGNED PART NUMBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE S
4、AE. PITCH DIAMETERS OF BOTH THREADED ENDS SHALL BE CONCENTRIC WITHIN .O06 FIR. (AMs 6320 MATERIAL MAY ALSO BE USED FOR THESE PARTS UNTIL. 1 JAN 1960.) 3 INSPECTION: ALL PARTS SHALL UNDERGO MAGNETIC INSPECTLON IN ACCORDANCE WITH AMS2640. PA 11 1 AIR FORCE-NAW AERONAUTICAL STANDARD AN 130499 THRU AN13
5、0774 CUST AV, AS 11 STUD - STRAIGHT, DRILLED, NECKED, .625-11 x .625-18 I I .US.PIYT .imao.n-i-:si-ii Project No. 5307-0365 K *us. THIS DOCUMENT CONTAINS - - PAGES. GOVERNMENT PRINTING OFFICE 1986 - 606438/43912 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
