1、MATERIAL IDENTJ- FICATJW ,010 Hm . o5 . o4 L!lHIS SURFACE MUST BE SQUARE WITH SHANK *xTlm: .oc; PLZL IhVICATOR READING (a) THIEAD TO HEAD. HAXIMUM TWO IMPERFECT IRPEADS. YOICI (1) THE IUNOUT FOR SIPAICHTNESS OF SHANK SHALL NOT EXCEED .O04 PIP PER INCH OF BOLT LEYGTE. (2) THE CONCENTRICITY OF THREAD
2、PD IN RELATION TO THE SUNK SHALL BE WITHIN .O06 FIR. (3) THE CONCENTRICITY OF THE NEXACON SOCKE1 IN RELATION TO OD OP HEAD SHALL BE YITUIN .O06 III. (4) THE CONCENTRICIIY DF THC SHANK IN RELATION TO OD OF HEAD SHALL BE WIIHXN .O05 FIE. HAIEIIAL: STEEL AHS 6322 PAIDYESS: ROCKWELL C32-36 FINISH: CADMI
3、UH PLAIE AMS 2400 SUIPACI IOUGHUESS: AS107 YIWUIACTURIIG SPEC1FICATIOH: AHS 7452 XNS?ECtIOYt ALL FAPTS SHALL UNDERGO MCNETIC INSPECIION IN ACCORDANCE WITH AHS2640. BXLAK SHARP EDGES .003-.015 UNLESS OTHERUISE SPECIFIED. DIMIUSIONS IN INCHES; UNLESS OTHERUXSE SPECIFIED: TOLERANCES; LINEAR DIHENSIOHS
4、t.010. ANGULAR DIHLHSIOKS ZZ . I PA 11 AIR FORCE-NAW AERONAUTICAL STANDARD AN148551 WRU BOLT - SOCKE1 HEAD, 6-HOLE DRILLSD. ,190-32 AN148650 DO MOT USE UNASSIGNED PART NUMBERS. INACTIVE FOR DESIGN AFTER I JAN 1960 SEE DRAWING LIS9080 For dafiaicion and application of drawing LPLUP notem) ab0 ANA Bullmtn HO. 337. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
