1、I l ANL0640L THRU ANLObSOO REV 3 53 = 7777735 0000274 T = - AIR FORCE-NAVY AERONAUTICAL STANDARD BOLT - CRES DRILLED HEX HEAD, 1 HOLE. .190-32 FED. SUP CLASS. I 5306 AN J 06 40 I ANI 8500 1.125 .500 1.189 .562 1.250 -625 AN106406 1.312 .688 ANl-O7 1.375 AN106408 1.438 AN106409 1.500 .E75 Aii106ir10
2、1.625 1.000 AN106012 1.875 1.950 Aii10641 2.000 1.375. Ul064lt 2.125 1.500 mioaii 1.750 1.125 PART 110. AR106415 AA106416 A11106418 A11106419 AN106420 An106421 AA106422 AA106423 A11106424 rmioc;si7 :;:29:2 106427 ANl06l+a AH lO&a +. O00 3 375 2 50 1064 0 3:500 I 2:&5 I A111064f6 3.625 3.000 AN106141
3、 3. 50 3.125 MlO6b42 3&5 3.250 Am06443 II (a) THREAD TO HEAD. HAXIHUH TWO IHPERFECT THREADS. NOTE: (r) SHANK SHALL BE STRAIGHT WITHIN .OO+ FIR. PER INCH OF BOLT LENGTH. . (2) TUE CONCENTRICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE HITHIN .O06 FIR. (31 THE CONCENTRICITY OF THE SHANK IN RELAT
4、LON TO THE HASHER FACE DIAMETER AND HEXAGON SHALL BE HITHIN .O11 FIR. INACTIVE FOR DESIGN AFTER 27 DEC i966 NO CUPERSEDINB STANDARD. MATERIAL: CORROSION RESISTANT STEEL - SEE HANUFACTURING SPECIFICATION SURFACE ROUGHNESS: AS107 . HANUFACTURiHG SPECIFICATION: AHS 7472 ) INSPECTION: ALL PARTS SHALL UN
5、DERGO FLUORESCENT PENETRANT INSPECTION IN ACCORDANCE WITH AUS2645. BREAK SHARP EDGES .003-.01S UNLESS OTHERWISE SPECIFIED. DIHENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLERANCES: LINEAR DIHENSIOHS 2.010. ANGULAR DIUENSIOHS 2 DO HOT USE UNASSIGNED PART NUHBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COHUITTEE OF THE CAE. P.A. Other CUSE USAF - II Navy - AS Army -AV I THIS DOCUMENT CONTAINS -.-.- PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
