1、 ANLOb30L THRU ANLO61100 REV 3 53 W 7777715 0000273 4 W FED. SUP CLASS. I 5306 HATERIAL IDENTIFICATION PER . AW2800. RAISED OR DEPRESSED r .o10 nu CHAMER 30 TO 1.062 DIA (OPPOSITE SIDE OPTIONAL) t 1.250 1.090 1.312 1.152 1.375 1.215 1-438 1.500 lS2s: 1.562 :O2 1.688 1.528 1.750 1.590 1.875 1.715 1.9
2、38 1.778 2.000 1.840 2.125 1.965 2.375 2.215 2.500 2.340 2.625 2.465 1.6 5 1.465 1.812 1.652 2.250 2.090 K +.o00 - .o60 .125 .188 .250 .312 .375 .438 .562 .625 .500 .688 - .750 .a12 a875 1.000 1.125 1.250 1.375 1.500 PART HO. 106306 n1063og aio63io AN10630 AN10630g AN106311 AN106312 AN106313 Arrio63
3、14 AN106315 AN106316 AN106317 AN106318 AN106319 AN106320 AN106321 AN106322 AR106323 L - 2.750 2.815 3.000 3.1 5 3.250 3.375 3.500 3.6 5 3.750 3.875 4,000 4.125 4.250 4.375 4.500 4.625 4:E 5.000 5.125 5.250 +.o00 2.590 1.625 2. 15 1.750 2.:go 5 5 15 5.590 6.000 5:LO UNIT MAY VARY FREELY 4.250 AN10634
4、5 4.375 AN106346 4.500 AN106347 4.625 AN106348 4. 50 AN106349 4. LINEAR DIMENSIONS 2.010, ANGULAR DO NOT USE UNASSIGNED PART NUHBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMHITTEE OF THE SAE. ) INSPECTION: ALL PARTS SHALL UNDERGO FLUORESCENT PENETRAN
5、T INSPECTION IN ACCORDANCE WITH AHS.2645. DIHENSIONS 2. P.A. AIR FORCE-NAVY AERONAUTICAL STANDARD AN I 0 630 I USAF - II Navy - AS Army - AV AN I cg400 Other Cust BOLT - CRES HEX HEAD, DRILLED SHANK, .750-16 I I YS 001TP-0111CL ,*l-I,-I,YIII1 Project No. 5306-1047 THIS DOCUMENT CONTAINS PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
